CN112258899A

CN112258899A - General aircraft longitude and latitude line network construction and operation control method

Info

Publication number: CN112258899A
Application number: CN202011131394.6A
Authority: CN
Inventors: 朱杰
Original assignee: Individual
Current assignee: Individual
Priority date: 2020-10-21
Filing date: 2020-10-21
Publication date: 2021-01-22
Anticipated expiration: 2040-10-21
Also published as: CN112258899B

Abstract

The invention discloses a construction and operation control method of a universal aircraft longitude and latitude air line network, which is characterized in that a monitoring airspace and a reporting airspace with the true height of 0-3000 m are distributed and divided into 5 cruise-level high airspaces according to a fixed wing aircraft, a helicopter, a self-rotating gyroplane, an electric multi-axis manned helicopter and a miniature electric multi-axis unmanned aerial vehicle, and a longitude air line is distributed on the upper layer of each level. The lower layer is distributed with weft routes, the course of each adjacent warp route and the course of each adjacent weft route are opposite, 5 grid graphs composed of the warp routes and the weft routes are formed in a monitoring airspace and a reporting airspace, and each graph is provided with a no-fly net hole and an airport, so that a national general aviation monitoring airspace and reporting airspace longitude and latitude route network is constructed, the national general aircrafts can orderly, safely and efficiently fly on the corresponding longitude and latitude routes at the same time, and the general aviation management department can realize high-quality service and safe, reliable, efficient, simple and convenient flight operation and monitoring management and control.

Description

General aircraft longitude and latitude line network construction and operation control method

Technical Field

The invention relates to a flight air management method of a low-altitude airspace general aircraft, in particular to a method for monitoring airspace and reporting airspace general aircraft airline operation and management and control, which is applied to the technical field of general aviation.

Background

The general aviation industry is a strategic emerging industry positioned by the country, the low-altitude airspace is a main area of general aviation activity, the management reform of the low-altitude airspace is deepened, the low-altitude airspace is an important measure for rapidly developing general aviation and flourishing the aviation industry, and the low-altitude airspace is an urgent need for promoting the development of the national economy and society. The united states is a general aviation country with 230000 registered general aviation airplanes and 19100 general aviation public and private airports. Since the construction cost of the general aviation airport is less than the construction cost of 2 kilometers of the highway, a large number of general airports distributed in various parts of the United states drive the development of small communities, and the gap between cities and villages is shortened. In the United states, the satellite navigation GPS is very reliable after being used and perfected for many years, and the satellite navigation GPS is widely used for navigation flight. The low-altitude visual chart used for navigation is rich in information, and in order to ensure the safety of navigation flight to the maximum extent, the information such as the sector safety height taking an airport as the center of a circle, the navigation and transportation airport distribution around the airport, the control communication demand, the remarkable terrain (mountains, rivers and high-voltage lines) and the like can be marked on the low-altitude chart in detail; information in aspects such as weather information, route information, destination airport information and the like can be acquired by using a smart phone. After the flight plan is made, the time from the notification of the empty pipe to the response is generally not more than 30 minutes.

In recent years, the general aviation industry in China has rapidly developed, and by 2018, more than 202 general airports exist, and 422 general aviation enterprises register 2415 general aircrafts. In 2018, 26 short-distance transportation routes are newly opened in China, but in general, the scale of the China general aviation industry is still small, the 'low altitude opening' is further accelerated, the general aviation traffic service function is highlighted, the general aviation market is vigorously cultivated, and a general aviation system which is reasonable in layout, convenient, rapid, advanced in manufacturing, safe and standard, wide in application and capable of being used by military and civilian is built. The method is mainly used for promoting the transformation and the upgrade of the industry, breaking the bottleneck restricting the development of the industry and promoting the all-round development of the general aviation industry.

The development targets published in China are that by 2020, more than 500 general airports are built, so that the situation that cities above the grade have the general airports or transport airports giving consideration to general aviation service basically is realized, and main agricultural product areas, main forest areas and more than 50% of 5A-grade tourist attraction areas are covered. The number of the general aircraft is more than 5000, and the economic scale of the general aviation in China is over 1 trillion yuan. The method has the advantages that the low-altitude airspace is expanded to be open, the low-altitude airspace with the original set true height of less than 1000 meters is expanded to realize the seamless connection between the monitoring airspace with the true height of less than 3000 meters and the reporting airspace, and the low-altitude visual flight route is drawn, so that the universal aircraft can fly fast and flexibly. Optimizing flight service, making a flight aeronautical chart, and improving the capabilities of low-altitude airspace aviation information, aviation meteorology, flight information and alarm service. The low-altitude airspace is divided into three types, namely a control airspace, a monitoring airspace and a reporting airspace.

The controlled airspace is generally set above areas with busy flight, such as airport taking-off and landing zones, air restricted zones, air dangerous zones, air restricted zones, ground important targets, national (border) zones, and the like. All airspace usage activities within this airspace must be approved and subject to flight control by the flight control department. The monitored airspace is usually arranged around a controlled airspace, all airspaces in the airspace use activities, and after an airspace user reports a flight plan to a flight control department, the airspace user can organize and implement the flight plan by self and is responsible for flight safety. The flight control department closely monitors airspace usage activity and provides flight intelligence services and alert services. The reporting airspace is generally arranged above areas far away from air restricted areas, air danger areas, national (border) border zones, ground important targets, and areas such as flight-dense areas and airport control areas. The users in the airspace can use the activities in all airspaces, and the users in the airspace can organize and implement the flight plan by themselves and take charge of the flight safety after reporting the flight plan to the flight control department, and the flight control department provides navigation information service according to the needs of the users.

In air defense safety, the flying height of the general aircraft is relatively low, the general aircraft is small in size, the flying speed is relatively low, the detection, the identification and the defense are difficult, if the low-altitude flight is not managed properly, the low-altitude aircraft or an unknown flyer is difficult to control, and if the low-altitude flight is released, the low-altitude flight is messy and has frequent accidents. Therefore, maintaining the order in the air and ensuring the safety are indispensable works.

The low-altitude airspace management reform published in China is divided into three stages: the first stage is trial-spotting, namely trial-spotting in Shenyang and Guangzhou flight control areas before 2011, and further accumulating experience; the second stage is popularization, namely, the achievement of trial point is popularized in China before 2015 years, and a low-altitude airspace operation management and service guarantee system with government supervision, industry guidance, market operation and national integration is basically formed; the third stage is deepening, namely before 2020, establishing a scientific air traffic control theory system, a regulation system, an operation management system and a service guarantee system, and realizing the full development and effective utilization of low-altitude air space domain resources.

General aviation refers to civil aviation activities except public aviation transportation by using civil aircrafts, including operation and flight in the industries of industry, agriculture, fishery and building, and flight activities in the aspects of medical health, emergency rescue, disaster relief, education training, cultural sports and the like, and a low-altitude airspace is a main area of general aviation activities and is an important strategic resource of the country. The manufacture of the general aircraft is not a bottleneck, because the general aircraft produced at home and abroad is various, some technologies are mature, and the training of flight drivers is not a bottleneck. How to fly orderly and safely, how to take off and land safely and efficiently, how to realize real-time monitoring and control is the main bottleneck restricting the development of general aviation in China, that is, the following can be concluded: 1. how to construct the network of routes for various aircraft in a generic aviation hierarchy, the routes comprising: course, heading, altitude, and time period. 2. How to construct an airport which is safe, efficient, simple and self-disciplined in taking off and landing in layout. 3. How to monitor and control the operation of the general aviation system in real time. The bottleneck problem of the construction of the general aviation route network. The general aviation aircraft can be divided into the following components according to the size of the body and the flying characteristics: 1. the medium and small fixed wing aircraft features high flying speed (400-600 km/h), large turning radius, long take-off and landing runway, need of relatively large airport, and suitability for long-distance trip between land-level intercity. 2. The maximum speed per hour of the small and medium-sized autorotation gyroplanes is 150 to 250 kilometers, the turning radius is small, the take-off and landing runway is short, a small airport is needed, the flight is safe and economical, and the small and medium-sized autorotation gyroplane is suitable for inter-city navigation in villages and towns, counties and ground levels. 3. The medium and small sized helicopters, with the maximum speed of 300-400 km/h, can take off and land vertically and hover in the air, have small required airports and large flying energy consumption, and are suitable for important or emergency flying activities. 4. The small electric multi-shaft manned helicopter has the advantages of low flying speed, maximum speed of 110 kilometers, capability of vertically taking off, landing and hovering, and only needs a very small airport, and is suitable for flying in urban areas or being used as an aerial taxi. 5. Miniature electronic multiaxis unmanned aerial vehicle, the flying speed is very slow, and the highest speed of time is 50 kilometers, can take off and land perpendicularly and hover, needs commodity circulation collection and distribution little airport, is fit for logistics system's express delivery. In summary, the general aircrafts have such many types, size, speed, range and take-off and landing characteristics, the use and use of the general aircrafts are greatly different, and a complex system with hundreds of thousands of or even millions of general aircrafts fly each day after the low altitude is opened, the general aircrafts need to keep orderly flying in a low altitude area with a seamless connection between a monitoring airspace and a reporting airspace below 3000 meters in true height without collision, and how to design and construct a flight network suitable, coordinated and combined with various general aircrafts is one of the most major bottlenecks for restricting the low altitude opening and the rapid development of the general aviation industry.

According to the standard of the existing airport arrangement, a left-handed take-off and landing mode is preferentially adopted, namely when the airplane takes off, the standard requires that all airplanes in the same airport take off and then fly off the airport after all airplanes take off and fly to the height required by the standard by adopting left-handed spiral rising in the airport. Similarly, the specification requires that all the airplanes entering the airport to land are landed to the airport in a left-handed spiral descending manner, that is, the take-off disc lift and the landing disc lift share a left-handed rectangular disc flying track. And the takeoff and landing share one runway, namely the front half section of the runway is used as a landing runway, and the rear half section is used as a takeoff runway. The take-off and the lifting of the aircraft and the landing of the aircraft are respectively used in a staggered time mode, the take-off and the landing of the aircraft are practical for a large airport with a tower for finely commanding the take-off and landing navigation, but the take-off and the landing of the aircraft are not practical for a general aviation airport, and because the take-off and the landing of the aircraft are busy, the technical requirement on the fine commanding, the take-off and the landing of the tower for finely commanding the navigation is high, the cost is high, and therefore how to construct the general aviation airport with safe, efficient, simple and self-. The bottleneck problem of how to operate and control the general aviation system is that after a low-altitude airspace is opened, general aircrafts flying every day in the country can quickly rise from tens of thousands of times to hundreds of thousands of times and finally to millions of times, general aviation management departments and companies need to monitor and control the flying state of each aircraft to different degrees, and how to operate and monitor and control is one of the most main bottlenecks of the opening of the low-altitude airspace.

The patent application number 201810229475, named as a navigation method of a general aviation aircraft, discloses a navigation method of the general aviation aircraft, which can provide a real-time dynamic aerial navigation map with step layering (0 to 3000 meters in height and one layering every 50 meters in height) for the aircraft through a plurality of sets of navigation monitoring systems covering a flight area arranged on a ground network and an airborne ip data transmission voice response radio station system arranged on the aircraft, so that the flight personnel can master the flight path and the surrounding flight situation in the air, and can know the flight safety track in real time; patent application No. 201410670313 discloses a navigation method, device and system of a general aviation aircraft, which relates to a navigation method, device and system of a general aviation aircraft, comprising: acquiring position information of a general aviation aircraft; reading in three-dimensional live-action data corresponding to the position information; acquiring a three-dimensional landscape low-altitude navigation data packet, wherein the three-dimensional landscape low-altitude navigation data packet comprises basic data, low-altitude obstacle data, threat area data and safety guarantee area data; the three-dimensional navigation live-action map is displayed according to the three-dimensional live-action data and the three-dimensional ground-action low-altitude navigation data packet, so that the flight safety of the low-altitude and ultra-low-altitude general aircraft can be effectively improved. The two latest inventions have the disadvantages that the course and the course of each flight of the aircraft are not fixed and random, and once the aircraft flies for more than dozens of times in the same airspace, the aircraft flies with each other inevitably, the pilot is highly stressed, the flight operation is considered to be lost, and the aircraft can collide with each other seriously. The existing technology for developing the general aviation industry is not strong in integrity, systematicness and practicability, and cannot bear the burden of promoting the general aviation industry as the development process of the national emerging strategic industry, so that how to improve the flight activity and the management and control capability of the general aircraft is proposed on schedule to solve the bottleneck problem.

Disclosure of Invention

In order to solve the problems of the prior art, the invention aims to overcome the defects in the prior art, and provides a method for constructing and operating and controlling a universal aircraft transit network, which is used for constructing a national universal aviation monitoring airspace and reporting airspace transit network, so that nationwide universal aircrafts can fly orderly, safely and efficiently on respective corresponding transit routes, and a universal aviation management department can realize high-quality service and safe, reliable, efficient, simple and convenient flight operation and monitoring and control.

In order to achieve the purpose, the invention adopts the following technical scheme:

a method for constructing and operating and controlling a universal longitude and latitude navigation network of an aircraft is characterized by comprising the following steps: according to a fixed wing airplane, a helicopter, a self-rotating gyroplane, an electric multi-shaft manned helicopter or a miniature electric multi-shaft unmanned aerial vehicle, a monitoring airspace and a reporting airspace of 0-3000 m of the true height of the airplane are divided into 5 cruise layer height airspaces; the cruise level airspace of the same type of general aircraft is divided into an upper layer and a lower layer; the upper layer layout of the same cruise floor high airspace is provided with warp routes at intervals, and the lower layer layout of the same cruise floor high airspace is provided with weft routes at intervals; or the upper layer layout of the same cruise layer high airspace sets weft routes at intervals, and the lower layer layout of the same cruise layer high airspace sets warp routes at intervals; defining a series of meridians in the monitoring airspace and the reporting airspace as flight paths of the aircraft from north to south or from south to north; and demarcating a series of wefts to be used as flight routes of the aircraft from east to west or west to east; the course of the adjacent meridian route and the course of the adjacent latitude route of the cruising level airspace of the same type of general aircraft are opposite to each other; 5 air line grid diagrams consisting of a series of meridian route and a series of latitude route are formed in a monitored airspace and a reported airspace, the side line of each grid is a route marked with a single course and a single height, and each grid is defined to be approximately square or rectangular; and each graph is provided with a no-fly net hole and an airport airspace, so that a general aviation monitoring airspace and a report airspace longitude and latitude navigation network are constructed;

for flight in the corresponding cruise level high altitude area, the amplitude of the up-and-down wave motion is limited, the following distribution division is made for the cruise flight level heights of 5 types of general aircraft of the monitoring airspace and the reporting airspace:

setting the height of 3000 m as the ground height of ground airport and the height of 0 m as the real height limit of monitoring airspace and reporting airspace;

setting a height airspace of (2800-2350 m) +/-200 m as a cruising layer height airspace of a small and medium-sized fixed wing aircraft carrying 1-20 passengers, wherein the side length of the applicable grid flight path is 5-15 km;

setting a height airspace of (2000-1750 m) + -100 m as a cruise floor height airspace of a helicopter carrying 1-20 passengers, wherein the side length of the applicable grid route is 0.5-2.0 km;

setting a height airspace of (1450-1150 m) ± 150 m as a cruising layer height airspace of a small and medium-sized autorotation rotorcraft carrying 1-20 passengers, wherein the side length of the suitable grid route is 1-3 km;

setting a height airspace of (400-250 meters) ± 50 meters as a cruising layer height airspace of the small manned electric multi-axis helicopter, wherein the side length of the applicable grid route is 200-600 meters;

setting a height airspace of (150-100 meters) ± 20 meters as a cruising layer height airspace of the miniature electric multi-axis unmanned aerial vehicle, wherein the side length of the applicable grid route is 25-50 meters;

when the aircraft actually cruises and flies, the flying height fluctuates up and down at the specified floor height, the invention limits the fluctuation value as above, can more fully utilize the airspace, and ensures the safety and the economic benefit; the method comprises the steps that related meridian routes and related latitude routes are disconnected and isolated at the outer sides of the boundary of a region where a longitude and latitude grid route is forbidden to fly in and fly over, and large and small isolated no-fly net holes are reserved on 5 route grid graphs of 5 related types of general aircrafts and are used for monitoring airspaces and reporting the flight operation and monitoring control of the airspace, an airport is arranged right below the airspace in one grid of the grid routes corresponding to various aircrafts, and a left-handed take-off and landing mode is preferably adopted according to the set specifications of the existing airport, or a right-handed take-off and landing mode is preferably adopted under special conditions;

at a proposed airport, selecting one grid from the air line grids corresponding to the take-off and landing positions of the airplane as the airport position, and constructing an airplane take-off and landing disk airport; the method comprises the following steps that a general aviation management department or an airline company distributes and divides cruising flight heights of 5 types of general aircrafts in a monitoring airspace and a reporting airspace from a true height of 3000-0 m on a managed electronic map, 5 longitude and latitude grid navigation networks can be generated in 5 layer height areas, the longitude and latitude grid navigation networks of a fixed wing aircraft, a self-rotating gyroplane and a helicopter can cover the monitoring airspace and the reporting airspace in most areas, the longitude and latitude grid navigation networks of an electric multi-axis manned helicopter and a miniature electric multi-axis unmanned aerial vehicle mainly cover the monitoring airspace and the reporting airspace in urban areas, each layer of network is provided with a network hole for isolating and controlling airspace, a no-fly zone, a flight obstacle zone and a temporary no-fly zone, and each layer of network is provided with a take-off and landing; therefore, the national and regional general aviation longitude and latitude grid navigation network for monitoring airspace and reporting airspace is constructed, each general aircraft is provided with a comprehensive navigator which is provided with a password and is suitable for the type of the corresponding aircraft, and the comprehensive navigator has the functions of an autopilot and bidirectional communication and automatic data transmission with a general aviation management department and an airline company besides navigation; when a user needs to fly to any airport from one airport of the same longitude and latitude navigation network, the user can apply for a general aviation management department or an airline company on the integrated navigator in real time, the general aviation management department and the airline company can display the optimal multiple air routes which can be selected after comprehensively considering factors including air route flight conditions and meteorological conditions on the integrated navigator in real time, the user can select one air route for flight in real time, relevant data of the aircraft flight states needing to be mastered by the general aviation management department and the airline company in the flight process are automatically transmitted to the general aviation management department and the airline company by the integrated navigator, once abnormal conditions including out-of-range flight and black flight occur, audible and visual alarms can occur on the electronic hierarchical display grid air route maps of the general aviation management department and the airline company, and the general aviation management department and the airline company can take corresponding measures, the general aviation management department and the airline company can transmit the flight guidance, prompt and warning information of the flight driver to the driver in real time, and can also carry out post-incident evaluation on the flight state data of the aircraft after the flight of the aircraft is finished, and carry out punishment and supervision management on illegal and illegal behaviors including border-crossing flight and black flight; the method comprises the following steps that an airplane flies according to a fixed longitude and latitude airline path, the flying environment from a takeoff airport to a landing airport and along the circumference of an airline is predicted, other general aircrafts are also predicted to orderly fly on respective longitude and latitude airlines simultaneously, an electronic landmark map or a three-dimensional electronic map of a ground scene along the airline is also predicted, and information transmission is realized by means of the three-dimensional electronic map or the electronic plane map of the ground scene provided by a satellite positioning navigation system and an autopilot on the general aircrafts; the flying of the longitude and latitude grid air route mainly takes instrument flying and automatic driving as the main part and visual flying as the auxiliary part.

As a preferred technical scheme of the invention, a fixed wing aircraft or a rotary wing aircraft left-hand double independent take-off and landing disk airport is arranged in a grid flight path with warp threads on the upper part and weft threads on the lower part, an airport is built in the center of the grid of the airport, two landing runways and two take-off runways are respectively and independently separated, a double isolation flight path design with a landing rectangular flight track and a lifting rectangular flight track which are respectively and independently separated is adopted, the two landing runways and the lifting rectangular flight track are respectively an independent subsystem, the two independent subsystems are mutually isolated and do not mutually interfere in operation, an airport terminal building is built in the center of the selected flight path grid, landing runways parallel to the warp threads are respectively arranged at set distances from the terminal building on the east side and the west side of the airport terminal building, the length and the width of the runways are implemented by technical parameters of the largest corresponding type of airplane type of landing model and the design specifications of the current runways, an east take-off runway is arranged in parallel with the east landing runway at a set distance from the east landing runway on the east landing runway, a west take-off runway is arranged in parallel with the west landing runway at a set distance from the west landing runway on the west landing runway, the length and width of the runways are implemented by technical parameters of the largest corresponding type of airplane model for taking off and design specifications of the existing runways, an east parking apron is arranged between the east landing runway and an airport terminal building, the airplane can turn to enter the east parking apron at the end of the landing runway after landing on the east landing runway, a west parking apron is arranged between the west landing runway and the airport terminal building, the airplane can turn to enter the west landing apron at the end of the west landing runway after landing on the west landing runway, and the central lines of the east landing runway and west landing runways extend to the north and set distances from grids, connecting the ends of two central lines, wherein the central lines of an east landing runway and a west landing runway simultaneously extend to the south to a set distance from a grid latitude line, and connecting the ends of the two central lines to form a rectangular landing flight track arranged in a route grid and can be shared by the east landing runway and the west landing runway; during taking off, the airplanes of the east-side parking apron and the west-side parking apron firstly drive into the take-off points of the east-side take-off runway and the west-side take-off runway respectively, after taking off, the airplanes respectively fly straight to the weft line and penetrate through the rectangular lifting flight track from the lower part of the weft line, after reaching the height of the weft line, the lifting flies in the weft line, and if necessary, the airplanes respectively lift from the weft line and the warp line to fly. In the selected left-handed flight path grid, a left-handed single independent take-off and landing disk airport is arranged, an airport terminal is built in the center of the selected grid by taking the layout of the left-handed double independent take-off and landing disk airport as a template, only an east landing runway, an east take-off runway and an east parking apron on the east side of the terminal are built or first-stage engineering is built, rectangular landing tracks and rectangular disk lifting tracks are reserved to form the left-handed east single independent take-off and landing disk airport, or the airport terminal is built in the center of the selected grid, only a west landing runway, a west landing runway and a west parking apron on the west side of the terminal are built or first-stage engineering is built, the rectangular disk lifting tracks and the rectangular disk lifting tracks are reserved to form the left-handed west single independent take-off and landing disk airport, a double-isolation flight path design that the disk lifting rectangular flight tracks and the disk lifting rectangular flight tracks are respectively and independently separated is formed, so that one rectangular landing runway and the disk lifting rectangular flight tracks form an independent subsystem, one takeoff runway and the lifting rectangular flight track form another independent subsystem, and the two independent subsystems are isolated from each other and do not interfere with each other in operation.

As a preferred technical scheme of the invention, a fixed wing aircraft or a rotary wing aircraft left-hand double independent take-off and landing disk airport is arranged in a grid flight path with upper latitude lines and lower longitude lines, an airport is built in the center of the grid of the airport, two landing runways and two take-off runways are respectively and independently separated, a double isolation flight path design with a landing rectangular flight track and a lifting rectangular flight track which are respectively and independently separated is arranged, the two landing runways and the lifting rectangular flight track are respectively an independent subsystem, the two independent subsystems are mutually isolated and do not mutually interfere in operation, an airport terminal building is built in the center of the selected flight path grid, landing runways parallel to the latitude lines are respectively arranged at set distances from the terminal building at the south side and the north side of the airport terminal building, the length and the width of the runways are implemented by technical parameters of the largest corresponding type of airplane type designed and the design specifications of the current runway, a south side take-off runway is arranged in parallel with the south side landing runway at a distance from the south side landing runway, a north side take-off runway is arranged in parallel with the north side landing runway at a distance from the north side landing runway, the length and width of the runways are implemented by the technical parameters of the largest corresponding type of airplane model for taking off and the design specifications of the current runways, a south side parking apron is arranged between the south side landing runway and the airport terminal building, the airplane can turn to enter the south side parking apron at the end of the landing runway after landing on the south side runway, a north side parking apron is arranged between the north side landing runway and the airport terminal building, the airplane can turn to enter the north side parking apron at the end of the north side runway after landing on the north side runway, the central lines of the south side landing runway and the north side runway simultaneously extend to an east distance grid at the longitude grid, connecting the ends of two central lines, wherein the central lines of a south landing runway and a north landing runway extend to the west at the same time and are away from the meridian of the grid by a set distance, and connecting the ends of the two central lines to form a rectangular landing flight track arranged in the airline grid for the south landing runway and the north landing runway; during taking off, the airplanes of the south side parking apron and the north side parking apron firstly drive into the flying points of the south side flying runway and the north side flying runway of the respective flying runways, the airplanes respectively fly straight to the longitude flight line after taking off and penetrate through the rectangular lifting flight track from the lower part of the longitude flight line, the lifting flight line enters the longitude flight line for flying after reaching the height of the longitude flight line, and then the airplanes respectively lift from the longitude flight line and enter the latitude flight line for flying if necessary. In the selected left-handed flight path grid, a left-handed single independent take-off and landing disk airport is arranged, an airport terminal is built in the center of the selected grid by taking the layout of the left-handed double independent take-off and landing disk airport as a template, only a south landing runway, a south take-off runway and a south parking apron on the south side of the terminal are built or first-stage engineering is built, rectangular landing tracks and rectangular disk lifting tracks are reserved to form a left-handed south independent stand-off aircraft field, or the airport terminal is built in the center of the selected grid, only a north landing runway, a north flying runway and a north parking apron on the north side of the terminal are built or first-stage engineering is built, the rectangular disk lifting tracks and the rectangular disk lifting tracks are reserved to form a left-handed north independent stand-off aircraft field, a double-isolated flight path design that the disk lifting rectangular flight tracks and the disk lifting rectangular flight tracks are respectively and independently separated is formed, so that one runway and the disk lifting rectangular flight tracks are automatically landed to form an independent subsystem, one takeoff runway and the lifting rectangular flight track form another independent subsystem, and the two independent subsystems are isolated from each other and do not interfere with each other in operation.

As a preferred technical scheme of the invention, a fixed wing airplane left-handed double independent take-off and landing disk airport is arranged in a flight path grid with warps on the upper portion and wefts on the lower portion to form a left-handed double independent take-off and landing disk airport layout, landing runways parallel to the warps are respectively arranged at positions 500-1000 m away from the east side and the west side of an airport terminal respectively in the center of a selected left-handed grid, the length and the width of each runway are executed by technical parameters of a designed landing maximum fixed wing airplane type and the design specifications of an existing runway, an east take-off runway is arranged in parallel with the east landing runway at the position 100-300 m away from the east landing runway at the east side of the east landing runway, a west take-off runway is arranged in parallel with the west landing runway at the position 100-300 m away from the west landing at the west side of the west landing, the length and the width of each runway are executed by the technical parameters of the designed maximum fixed wing airplane type and the design specifications of the existing runway, an east parking apron is arranged between the east landing runway and the station building, the airplane enters the east parking apron after the east landing runway lands, the tail end of the landing runway turns, a west parking apron is arranged between the west landing runway and the station building, and the airplane enters the west parking apron after the west landing runway lands, and the tail end of the west landing runway turns; two end parts of two central lines are respectively formed at the positions of central lines of the east landing runway and the west landing runway extending to the south and the north simultaneously and 500-1000 meters away from the weft route, wherein the central lines comprise the north end and the south end of the east landing runway and the north end and the south end of the west landing runway, a route parallel to the weft route respectively connects the north end and the south end of the two central lines to form a rectangular landing flight track which is shared by the east landing runway and the west landing runway, when an airplane lands, the airplane flying on the weft route directly cuts into the landing flight track, the airplane flying on the warp route firstly descends to the weft route and then cuts into the landing flight track, the weft route and the warp route form 4 sides of a grid route, the landing flight track is arranged at the outer sides of the 4 sides of the grid route, an outer side route is formed at a position 100-600 meters away from the side line of the grid route, and the 4 corners of the outer side route are in transitional connection in a circular arc, forming a disk-lifting flight track for sharing the east-rising runway and the west-rising runway; during taking off, the airplanes of the east parking apron and the west parking apron firstly drive into the flying starting points of the east take-off runway and the west take-off runway which respectively correspond to the east take-off runway, the airplanes respectively directly fly the weft line after taking off and penetrate through the rectangular lifting flying track from the lower part of the weft line, and the weft line flies after the lifting reaches the height of the weft line; or, the aircraft respectively ascends from the latitude line and flies in the longitude line;

or preferably, a fixed-wing aircraft left-handed single independent take-off and landing disk airport is set, a layout drawing of a left-handed double independent take-off and landing disk airport is taken as a template, an airport terminal is established in the center of a selected left-handed grid, and the airport terminal is in the grid of the selected left-handed flight path;

or preferably, a left-handed single independent take-off and landing disk airport is set, a layout drawing of the left-handed double independent take-off and landing disk airport is taken as a template, an airport terminal is established in the center of a selected grid, only an east landing runway, an east take-off runway and an east parking apron on the east side of the terminal are established or first-stage engineering is established, and a rectangular take-off and landing disk airport is formed by reserving a rectangular take-off and landing disk track and a rectangular take-off and landing disk track;

or preferably, an airport terminal building is built in the selected grid center, only a west landing runway, a west departure runway and a west parking apron on the west side of the terminal building are built or first-stage engineering is built, and the rectangular disc lifting track are reserved to form the levogyration west single independent take-off and landing disc airport.

As a preferred technical scheme of the invention, a left-handed double independent take-off and landing disk airport of the autorotation gyroplane is arranged in a flight path grid with warp threads on the upper part and weft threads on the lower part, a layout of the left-handed double independent take-off and landing disk airport of the autorotation gyroplane is formed, a terminal building is established in the center of a selected left-handed grid, landing runways parallel to the warp threads are respectively arranged at positions 100-300 meters away from the terminal building on the east side and the west side of the terminal building, the length and the width of the runways are executed by technical parameters of the maximum autorotation gyroplane type designed to land and the design specification of the existing runways, an east take-off runway is arranged in parallel with the east landing runway at the position 50-100 meters away from the west landing runway on the east side of the east landing runway, a west take-off runway is arranged in parallel with the west landing runway, the length and the width of the runway are executed by technical parameters of the maximum autorotation gyroplane type designed and the design specification of the existing, an east parking apron is arranged between the east landing runway and the station building, the airplane enters the east parking apron after landing on the east landing runway, the west parking apron is arranged between the west landing runway and the station building, and the airplane enters the west parking apron after landing on the west landing runway; two end parts of two central lines are respectively formed at positions which simultaneously extend to south and north from the central lines of the east landing runway and the west landing runway and are 100-300 meters away from the latitude line, wherein the two end parts comprise the north end and the south end of the east landing runway and the north end and the south end of the west landing runway, a route parallel to the latitude line respectively connects the north end and the south end of the two central lines to form a rectangular landing flight track which is shared by the east landing runway and the west landing runway, when an airplane lands, the airplane flying on the latitude line can directly cut into the landing rectangular flight track, the airplane flying on the longitude line firstly descends to the latitude line and then cuts into the landing rectangular flight track, the latitude line and the longitude line form 4 edges of a grid, the landing flight track is arranged at the outer side of the 4 edges of the grid line, an outer side line is formed at a distance of 100-200 meters from the edge line of the grid line, and 4 corners of the outer side arc line are in transitional connection in a form, forming a lifting rectangular flight track for the east and west lifting runways to share, wherein during lifting, the autorotation gyroplanes of the east and west parking aprons firstly drive into the lifting points of the east and west lifting runways corresponding to the lifting runways respectively, after the aircraft lifts, the aircraft respectively directly flies on the weft flight lines and passes through the lifting rectangular flight track cut into the lifting rectangular flight track from the bottom of the aircraft, and after the lifting reaches the height of the weft, the aircraft enters the weft flight lines for flying, or after the lifting reaches the height of the weft flight lines, the aircraft respectively lifts on the weft flight lines and flies on the warp flight lines;

or preferably, a left-handed single independent take-off and landing disk airport of the autorotation gyroplane is set, an airport terminal building is built in the center of the selected grid by taking a layout drawing of the left-handed double independent take-off and landing disk airport of the autorotation gyroplane as a template, an east landing runway, an east take-off runway and an east parking apron on the east side of the terminal building are built only or first-stage engineering is built, and a rectangular disk landing track and a rectangular disk lifting track are reserved to form the left-handed east single independent take-off and landing disk airport of the autorotation gyroplane;

or preferably, an airport terminal building is built in the selected grid center, only a west landing runway, a west departure runway and a west parking apron on the west side of the terminal building are built or first-stage projects are built, rectangular disk lifting tracks and rectangular disk lifting tracks are reserved, and a rotary gyroplane left-handed western single independent take-off and landing disk airport is formed.

As a preferred technical scheme of the invention, a fixed wing airplane left-handed double independent take-off and landing disk airport is arranged in a flight path grid with weft threads on the upper part and warp threads on the lower part, a fixed wing airplane left-handed double independent take-off and landing disk airport layout is formed, a terminal building is established in the center of a selected left-handed grid, landing runways parallel to the weft threads are respectively arranged at the positions 500-1000 meters away from the terminal building on the south side and the north side of the terminal building, the length and the width of the runways are executed by the technical parameters of the designed largest fixed wing airplane type landing and the design specifications of the existing runways, a south take-off runway is arranged in parallel with the south landing runway at the position 100-300 meters away from the north landing runway, a north take-off runway is arranged in parallel with the north landing runway at the position 100-300 meters away from the north landing runway, the length and the width of the runways are executed by the technical parameters of the designed largest fixed wing airplane type and the design specifications of the existing runways, a south parking apron is arranged between the south landing runway and the station building, after the airplane descends on the south landing runway, the airplane enters the south parking apron by turning at the end of the landing runway, a north parking apron is arranged between the north landing runway and the station building, after the airplane descends on the north landing runway, the airplane enters the north parking apron by turning at the end of the north landing runway; two end parts of two central lines are respectively formed at the positions of central lines of a south landing runway and a north landing runway, which simultaneously extend towards the east and west directions and are 500-1000 meters away from grid meridian lines, wherein the two end parts comprise the east end and the west end of the south landing runway and the east end and the west end of the north landing runway, and a parallel weft line air route grid meridian line respectively connects the east end and the west end of the two central lines to form a rectangular landing flight track for the south and north landing runways, when an airplane lands, the airplane flying on a meridian line directly lands on the landing flight track, the airplane flying on a weft line needs to firstly descend to the meridian line and then cut into a landing flight track, the weft line and the warp line form 4 edges of the grid, the landing flight track is arranged at the outer sides of the 4 edges of the air route grid air route, an outer side air route is formed at the position 100-600 meters away from the edge line of the air route grid air route, and 4 corners of the outer side air route are, a disk-lifting rectangular flight track is formed and is shared by the south-rising runway and the north-rising runway; during taking off, the airplanes of the south parking apron and the north parking apron firstly run into the flying points of the south taking-off runway and the north taking-off runway respectively, the airplanes respectively fly straight to the longitude route and penetrate through the rectangular lifting flying track from the lower part of the longitude route after taking off, and the lifting flies in the longitude route after reaching the longitude height; or, the aircraft respectively ascends from the meridian route and flies in the latitude route;

or preferably, a fixed-wing airplane left-handed single independent take-off and landing disk airport is arranged in a selected left-handed airline grid, an airport terminal is established in the center of the selected grid by taking a fixed-wing airplane left-handed double independent take-off and landing disk airport layout picture as a template, a south landing runway, a south take-off runway and a south parking apron on the south side of the terminal are only built or first-stage engineering is firstly built, rectangular disk landing tracks and rectangular disk lifting tracks are reserved, and the fixed-wing airplane left-handed south independent take-off and landing disk airport is formed;

or preferably, an airport terminal building is built in the selected grid center, only the north landing runway, the north flying runway and the north parking apron on the north side of the terminal building are built or first-stage projects are built, the rectangular disc landing track and the rectangular disc lifting track are reserved, and the fixed-wing airplane left-hand and north-hand independent landing disc airport is formed.

As a preferred technical scheme of the invention, an autorotation gyroplane left-handed double independent take-off and landing disk airport is arranged in a flight path grid with weft threads above and warp threads below, a layout of the autorotation gyroplane left-handed double independent take-off and landing disk airport is formed, a terminal building is established in the center of a selected left-handed grid, landing runways parallel to the weft threads are respectively arranged at positions 100-300 meters away from the terminal building on the south side and the north side of the terminal building, the length and the width of each runway are executed by technical parameters of the designed maximum autorotation gyroplane type and the design specifications of the existing runways, a south take-off runway is arranged parallel to the south landing runway at a position 50-100 meters away from the north landing runway, a north take-off runway is arranged parallel to the north landing runway, the length and the width of each runway are executed by technical parameters of the designed maximum autorotation gyroplane type and the design specifications of the existing runways, a south parking apron is arranged between the south landing runway and the station building, after the airplane descends on the south landing runway, the airplane enters the south parking apron by turning at the end of the landing runway, a north parking apron is arranged between the north landing runway and the station building, after the airplane descends on the north landing runway, the airplane enters the north parking apron by turning at the end of the landing runway; the method comprises the steps that two end parts of two central lines are formed at positions, which are 100-300 meters away from grid warps, of central lines of a south landing runway and a north landing runway and simultaneously extend towards the east and west directions, wherein the positions comprise the east end and the west end of the south landing runway and the east end and the west end of the north landing runway; the latitude line and the longitude line form 4 sides of a grid line, the lifting flight track is arranged on the outer side of the 4 sides of the grid line, an outer side line is formed at a position which is 100-200 meters away from the line from the side line of the grid line, 4 corners of the outer side line are in transitional connection in the form of an arc line to form a lifting rectangular flight track for sharing the south lifting runway and the north lifting runway, during take-off, autorotation rotorcraft of the south parking apron and the north parking apron firstly drive into respective take-off runway south take-off runway and north lifting runway flying points, after the aircraft takes off, the aircraft respectively flies straight through the longitude line and passes through the lifting rectangular flight track from the lower part of the takeoff runway to be cut into the lifting rectangular flight track, and after the lifting reaches the height of the longitude line, the lifting flight; or, the aircraft respectively ascends from the meridian route and flies in the latitude route;

or preferably, in the selected left-handed airline grid, setting a self-rotary-wing aircraft left-handed single independent take-off and landing disk airport, taking a self-rotary-wing aircraft left-handed double independent take-off and landing disk airport layout picture as a template, establishing an airport terminal in the center of the selected grid, only establishing or first-stage engineering firstly establishing a south landing runway, a south take-off runway and a south parking apron on the south side of the terminal, and reserving a rectangular disk lifting track and a rectangular disk lifting track to form the self-rotary-wing aircraft left-handed south independent stand-up landing disk airport;

or preferably, an airport terminal building is built in the selected grid center, only the north landing runway, the north flying runway and the north parking apron on the north side of the terminal building are built or first-stage projects are built, the rectangular disk lifting track and the rectangular disk lifting track are reserved, and the independent left-handed and north-handed vertical landing disk airport of the autogyro is formed.

As a preferred technical scheme of the invention, in any one of 5 airline grid maps corresponding to 5 types of general aircrafts, controlled airspace, national major engineering area, flight obstacle area, tourist attraction area, free flight area, temporary no-fly area, permanent and temporary no-fly airspace are arranged in the isolation net hole where no-fly and no-fly are allowed; the controlled airspace comprises a military no-fly zone; the national major engineering area comprises areas of nuclear power stations, major hydraulic engineering and large airports; the flight obstacle area comprises high-outburst terrains, ultrahigh buildings, overhead power transmission line towers and areas where wind driven generators are located; the tourist attraction comprises airspace where the scenic attraction is organized such as aircraft flight, fire balloon flight, flight wing flight and unmanned aerial vehicle flight activity; the free flight area is an airspace specially set by general aviation enthusiasts for coach flight, entertainment flight and free dazzling and technical performance; the temporary no-fly area comprises an aviation exhibition flight performance area, a disaster rescue area and an air target ground danger area of military performance.

The airport is arranged in a route grid, and the size and the arrangement of the airport are closely related to the size of a general aircraft model, the take-off and landing distance, the vertical take-off and landing and hovering characteristics and the heading arrangement combination of 4 sidelines of the route grid.

Airport setup for fixed-wing aircraft: the airport is arranged in a grid with the size corresponding to the airport, a left-handed take-off and landing mode is preferentially adopted according to the specification of the existing airport arrangement, namely, when the airplane takes off, the specification requires that all airplanes in the same airport take off, and then fly off the airport after all airplanes in the same airport take off and fly to the height required by the specification by adopting left-handed spiral rising. Similarly, the specification requires that all the airplanes entering the airport to land to the airport by adopting a left-handed spiral descending mode, the airplanes in the prior art share a runway for taking off and landing, the front half section of the airplanes serves as a landing runway, the rear half section of the airplanes serves as a taking off runway, and the planes in the prior art also share a rectangular disk flying track for taking off and landing, so that the planes in the prior art cannot take off and lift up when landing and landing, and similarly, the planes cannot fall off and land when starting and landing, and the time for taking off and landing must be staggered. The invention considers that the general aviation fixed wing aircraft airport in the monitoring airspace and the reporting airspace is much smaller than the main aircraft airport, the model is much smaller, but the number of the flying aircraft is much more than the main airport every day, and the equipment level of the airport configuration and the number configuration and the technical level of the management personnel are far lower than the main airport, in order to reduce the operating cost of the airport, the safe, efficient, reliable, simple and convenient and self-discipline operation of the general aviation fixed wing aircraft airport is realized, the invention provides a double-isolation technology that the landing runway is separated from the runway, the landing rectangular flying orbit is separated from the lifting rectangular flying orbit, the landing rectangular flying orbit and the lifting rectangular flying orbit form an independent subsystem, and the landing runway and the lifting rectangular flying orbit form an independent subsystem, the two independent subsystems are isolated from each other, and the operation is not interfered with each other, so that a single independent take-off and landing disk flying left-handed fixed wing aircraft airport is formed. In order to further improve the efficiency, the invention also provides a technical scheme that two landing runways share one rectangular take-off and landing flight track and two take-off runways share one rectangular take-off and landing flight track, thereby forming a double-independent take-off and landing disk left-handed fixed wing aircraft airport. It is also specified in the current airport construction specifications that, in special cases, right-handed airports may also be used, where right-handed airline grids are selected for airport construction.

Setting of helicopter airports: setting of the helicopter airport: due to the characteristic that the helicopter can take off and land vertically and hover, one grid can be selected as an airport according to model corresponding air route grids at the proposed airport, and the airport is built according to the existing specifications.

The setting of the autorotation gyroplane airport preferentially adopts a left-handed taking-off and landing mode according to the set standard of the existing airport, and the grid with the left-handed flight line is selected from the corresponding flight line grids at the proposed airport according to the autorotation gyroplane. It is also specified in the current airport construction specifications that, in special cases, right-handed airports may also be used, where right-handed airline grids are selected for airport construction.

The setting of electronic multiaxis manned helicopter airport: due to the characteristic that the electric multi-axis helicopter can vertically take off and land and hover, one of the flight line grids corresponding to the model of the planned airport can be selected as the airport, and the airport can be built according to the existing specification of the helicopter.

Airport setting of miniature electronic multiaxis unmanned aerial vehicle: the design is carried out according to the use purpose and by referring to the helicopter airport construction specification.

The general aircraft flight rules are basically applied to the existing flight rules, and the invention supplements the following:

and arranging the general aircraft in flight passages of the warp line and the weft line. Setting a straight forward flight path on the meridian flight path and the latitude flight path according to the specified layer height as an overtaking flight path, and respectively setting a same high-layer cruise path flying in the same direction on the left side and the right side of the overtaking flight path. Overrunning flight: when the airplane flying on the left cruise channel exceeds the front airplane, the airplane can change the channel to the overtaking channel to accelerate, and after the airplane crosses the front airplane of the left cruise channel or the right cruise channel for a safe interval distance, the airplane can change the channel to the left cruise channel or change the channel to the right cruise channel. When the airplane flying on the right cruise channel exceeds the front airplane, the airplane can change the channel to the overtaking channel to accelerate, and after the airplane crosses the right cruise channel or the front airplane of the left cruise channel for a safe spacing distance, the airplane can change the channel to the right cruise channel or change the channel to the left cruise channel. The overtaking channel is only used for overtaking flight, and the channel is changed to the patrol channel in time after the overtaking flight is finished.

The invention realizes the construction of a national monitoring airspace and reporting airspace general aviation longitude and latitude grid navigation network, and general aviation management departments and airlines distribute and divide the cruising flight height of 5 types of general aircrafts on a managed electronic map or an electronic three-dimensional map from the true height of 3000 meters to 0 meter to generate 5 layer height areas corresponding to the cruising flight of the aircrafts. Similar 5 floor height areas can generate 5 longitude and latitude grid air lines, the longitude and latitude grid air lines of the fixed-wing aircraft, the autorotation gyroplane and the helicopter can cover most of the monitoring airspace and the reporting airspace of the homeland, and the longitude and latitude grid air lines of the electric multi-shaft manned helicopter and the miniature electric multi-shaft unmanned aerial vehicle mainly cover urban areas. Net holes for isolating a no-fly area and a flight obstacle area are reserved on each layer of the net, and a take-off and landing airport is arranged on each layer of the net. Therefore, a huge, hierarchical and three-dimensional national general aviation monitoring airspace and reporting airspace longitude and latitude grid navigation network is constructed.

Compared with the prior art, the invention has the following obvious and prominent substantive characteristics and remarkable advantages:

1. the method of the invention constructs the national and regional monitoring airspace and reporting airspace general aviation longitude and latitude grid navigation network, covers the flight activities and the control of almost all general aircrafts in the monitoring airspace and the reporting airspace, provides an integral, systematic and practical implementation scheme for the opening of the national low-altitude airspace and the vigorous development of the general aviation industry, and can further accelerate the progress of the general aviation industry as the development of the national strategic industry;

2. the biggest difference between the invention and the comparison technology is that the general aircraft flies according to fixed longitude and latitude airline paths in a monitoring airspace and a reporting airspace, the flying environments (airlines, terrains, meteorology, obstacles, no-fly areas, net holes and the like) from a takeoff airport to a landing airport and along the periphery of the airlines are all known, other general aircraft orderly fly on the longitude and latitude airlines of the monitoring airspace and the reporting airspace are also known, the plane electronic terrain landmark map or the three-dimensional ground view electronic map along the route is also predicted, the sudden collision event is prevented from everywhere and in real time, the system is particularly suitable for instrument flight and automatic driving, and can be realized by means of a three-dimensional landscape electronic map or an electronic plane map provided by a Beidou satellite positioning navigation and a high-resolution satellite and an automatic pilot on a general aircraft; the invention relates to a longitude and latitude grid air route, which mainly takes instrument flight and automatic driving as main flight and takes visual flight as auxiliary flight;

3. the method greatly improves the flight safety of the general aircraft, 5 types of general aircraft are distributed in 5 layered airspaces of a monitoring airspace and a reporting airspace, each layered airspace is divided into an upper cruising flight level and a lower cruising flight level, the upper level is distributed with a warp flight line, the lower level is distributed with a weft flight line, or the upper level is distributed with a weft flight line, the lower level is distributed with a warp flight line, and 10 levels with different heights are used for 5 types of general aircraft to cruise and fly; the flight safety distance is reserved between every two layers and every two air routes, the flight of every two air routes is not interfered with each other, all general aircrafts in the whole general aviation longitude and latitude grid air route fly in order, and the aircrafts cannot collide with each other, so that the safety is high; the longitude and latitude grid airline network is also provided with large and small isolation mesh holes, so that safety guarantee is provided for the aircraft to avoid colliding with obstacles and fly around a no-fly zone; safety is the first important to flight, and the general aviation industry can develop rapidly only by realizing flight safety;

4. the invention provides a construction and operation control method of a general aviation longitude and latitude grid navigation network, the longitude and latitude grid navigation network can cover most of the monitoring airspace and the reporting airspace of the territory, and nationwide general aircraft navigation can be realized;

5. the whole network of the method can accommodate the flight activities of hundreds of thousands of universal aircrafts to millions of universal aircrafts, and is very efficient; the universal aircraft flies according to the fixed longitude and latitude air route, is particularly suitable for instrument flight and automatic driving, improves the flight safety and reduces the control intensity of pilots;

6. the method of the invention provides guidance and basis for airport site selection and construction of different types of general aircrafts: the fixed-wing aircraft and the autorotation gyroplanes preferentially build an airport in a left-handed airline grid, and by adopting the airport building scheme of the invention, two landing runways share one landing rectangular track and two taking-off runways share one lifting rectangular track, the safe, efficient, reliable, simple and convenient and autonomous operation of the airport can be ensured; the single independent take-off and landing disk airport provides a preferable scheme for the construction of airports in remote areas and the first-stage construction of potential busy airports, and can be constructed in two steps and then completely constructed in the second stage; helicopters, electric multi-shaft manned helicopters and miniature electric multi-shaft unmanned aerial vehicle airports can be arranged in any airline grid, and take-off and landing are based on the construction specifications of the helicopter airport;

7. the pilot of the invention approves and provides a plurality of preferred alternative routes from declaring a flight route to a general aviation management department and an airline company, the response speed is very fast, the response speed can be realized within a few seconds, the efficiency is greatly improved compared with that from declaring to approving at present, the time is several weeks long, the time is several days short, and the time is dozens of minutes fast, the response speed is much faster even than the time of using in the United states for 30 minutes, the efficiency is very high, because the longitude and latitude routes are all preset, the airport is also preset, and the computer only needs to preferably approve and reply according to the weather condition of the route and the busy condition of the route;

8. the method of the invention enables the general aviation management department and the airline company to provide various services for the general aircraft users: establishing a national monitoring airspace and reporting airspace general aviation network system, providing a preferred air route in real time for a user to select, providing meteorological service, flight guidance, prompting and warning; the method of the invention enables general aviation management departments and airlines to monitor and control the flight activities of all general aircrafts in real time through the bidirectional transmission of flight data, thereby realizing the comprehensive control of the real-time declaration and real-time approval of the flight activities in advance, the real-time monitoring and real-time control in the process and the post-evaluation treatment.

Drawings

FIG. 1 is a schematic diagram of the layered configuration of the transit grid routes of a general aircraft for monitoring and reporting airspace in real height of 0 to 3000 meters.

FIG. 2 is a plan view of a transit grid route for a fixed wing aircraft of the present invention.

Fig. 3 is a top view of a transit grid pattern of a rotorcraft according to the present invention.

Fig. 4 is a schematic view of a layout of a fixed-wing aircraft left-handed dual independent take-off and landing disk airport with warps on the top and wefts on the bottom route grid according to a fourth embodiment of the invention.

Fig. 5 is a schematic view of a fixed-wing aircraft east-left-handed single independent take-off and landing disk airport layout with warp threads in the upper and weft threads in the lower flight path grid according to a fourth embodiment of the present invention.

Fig. 6 is a schematic view of a fixed-wing aircraft west-left-handed independent take-off and landing disc airport layout with warp threads in the upper and weft threads in the lower flight path grid according to a fourth embodiment of the present invention.

Fig. 7 is a schematic view of a left-handed dual independent take-off and landing disk airport layout of a gyroplane with warp threads on the top and weft threads in a grid of a lower flight path according to a fifth embodiment of the present invention.

Fig. 8 is a schematic view of a layout of a fixed-wing aircraft left-handed dual independent take-off and landing disk airport with its latitude lines up and longitude lines in a lower flight path grid according to a sixth embodiment of the present invention.

Fig. 9 is a schematic view of a left-handed dual independent take-off and landing disk airport layout of a rotorcraft with its weft threads up and its warp threads down according to a seventh embodiment of the present invention.

Detailed Description

The above-described scheme is further illustrated below with reference to specific embodiments, which are detailed below:

the first embodiment is as follows:

in the embodiment, referring to fig. 1, a method for controlling the construction and operation of a universal aircraft transit network is to divide a monitoring airspace and a reporting airspace of 0-3000 m in true height of an aircraft into 5 cruise-level high airspaces according to a fixed-wing aircraft, a helicopter, a self-rotating gyroplane, an electric multi-axis manned helicopter or a miniature electric multi-axis unmanned aerial vehicle; the cruise level airspace of the same type of general aircraft is divided into an upper layer and a lower layer; the upper layer layout of the same cruise floor high airspace is provided with warp routes at intervals, and the lower layer layout of the same cruise floor high airspace is provided with weft routes at intervals; or the upper layer layout of the same cruise layer high airspace sets weft routes at intervals, and the lower layer layout of the same cruise layer high airspace sets warp routes at intervals; defining a series of meridians in the monitoring airspace and the reporting airspace as flight paths of the aircraft from north to south or from south to north; and demarcating a series of wefts to be used as flight routes of the aircraft from east to west or west to east; the course of the adjacent meridian route and the course of the adjacent latitude route of the cruising level airspace of the same type of general aircraft are opposite to each other; 5 air line grid diagrams consisting of a series of meridian route and a series of latitude route are formed in a monitored airspace and a reported airspace, the side line of each grid is a route marked with a single course and a single height, and each grid is defined to be approximately square or rectangular; and each graph is provided with a no-fly net hole and an airport airspace, so that a general aviation monitoring airspace and a report airspace longitude and latitude navigation network are constructed;

the method comprises the steps that related meridian routes and related latitude routes are disconnected and isolated at the outer sides of the boundary of a region where a longitude and latitude grid route is forbidden to fly in and fly over, including a controlled airspace, a flight obstacle area and a temporary flight forbidding area, and large and small isolated fly forbidding tunnels are reserved on 5 route grid graphs of 5 related types of general aircrafts and are used for monitoring the airspace and reporting the flight operation and monitoring control of the airspace, an airport is arranged right below the airspace in one grid of the grid routes corresponding to various aircrafts, a left-handed take-off and landing mode is adopted according to the set specifications of the existing airport, and a right-handed take-off and landing mode is also adopted under special conditions;

In this embodiment, the fixed-wing aircraft is a fixed-wing aircraft, as shown in fig. 1, the upper layer is 2800 meters high, the warp routes 10 are laid out, the distance between every two adjacent warp routes is 5-15 kilometers, and the directions of every two adjacent warp routes are opposite to each other. The height of the lower layer is 2350 m, the weft air lines 11 are distributed, the interval distance between every two adjacent weft air lines is 5-15 km, and the directions of every two adjacent weft air lines are opposite to each other.

Example two:

this embodiment is substantially the same as the first embodiment, and is characterized in that:

in the embodiment, a fixed wing airplane or a rotary wing aircraft left-hand double independent take-off and landing disk airport is arranged in a grid flight path with warp threads on the upper part and weft threads on the lower part, an airport is built in the center of the net grid of the airport, two landing runways and two take-off runways are respectively and independently separated, a double isolation flight path design with a landing rectangular flight track and a lifting rectangular flight track which are respectively and independently separated is adopted, the two landing runways and the lifting rectangular flight track are respectively an independent subsystem, the two independent subsystems are mutually isolated and do not mutually interfere in operation, an airport terminal building is built in the center of the selected flight path grid, a runway parallel to the landing of the warp threads is respectively arranged at the east side and the west side of the airport terminal building at set distances from the terminal building, the length and the width of the runway are implemented by the technical parameters of the largest corresponding type of airplane with the designed type landing of the warp threads and the design specifications of the current runway, an east take-off runway is arranged in parallel with the east landing runway at a set distance from the east landing runway on the east landing runway, a west take-off runway is arranged in parallel with the west landing runway at a set distance from the west landing runway on the west landing runway, the length and width of the runways are implemented by technical parameters of the largest corresponding type of airplane model for taking off and design specifications of the existing runways, an east parking apron is arranged between the east landing runway and an airport terminal building, the airplane can turn to enter the east parking apron at the end of the landing runway after landing on the east landing runway, a west parking apron is arranged between the west landing runway and the airport terminal building, the airplane can turn to enter the west landing apron at the end of the west landing runway after landing on the west landing runway, and the central lines of the east landing runway and west landing runways extend to the north and set distances from grids, connecting the ends of two central lines, wherein the central lines of an east landing runway and a west landing runway simultaneously extend to the south to a set distance from a grid latitude line, and connecting the ends of the two central lines to form a rectangular landing flight track arranged in a route grid and can be shared by the east landing runway and the west landing runway; during taking off, the airplanes of the east-side parking apron and the west-side parking apron firstly drive into the take-off points of the east-side take-off runway and the west-side take-off runway respectively, after taking off, the airplanes respectively fly straight to the weft line and penetrate through the rectangular lifting flight track from the lower part of the weft line, after reaching the height of the weft line, the lifting flies in the weft line, and if necessary, the airplanes respectively lift from the weft line and the warp line to fly. In the selected left-handed flight path grid, a left-handed single independent take-off and landing disk airport is arranged, an airport terminal is built in the center of the selected grid by taking the layout of the left-handed double independent take-off and landing disk airport as a template, only an east landing runway, an east take-off runway and an east parking apron on the east side of the terminal are built or first-stage engineering is built, rectangular landing tracks and rectangular disk lifting tracks are reserved to form the left-handed east single independent take-off and landing disk airport, or the airport terminal is built in the center of the selected grid, only a west landing runway, a west landing runway and a west parking apron on the west side of the terminal are built or first-stage engineering is built, the rectangular disk lifting tracks and the rectangular disk lifting tracks are reserved to form the left-handed west single independent take-off and landing disk airport, a double-isolation flight path design that the disk lifting rectangular flight tracks and the disk lifting rectangular flight tracks are respectively and independently separated is formed, so that one rectangular landing runway and the disk lifting rectangular flight tracks form an independent subsystem, one takeoff runway and the lifting rectangular flight track form another independent subsystem, and the two independent subsystems are isolated from each other and do not interfere with each other in operation. As shown in fig. 2, a grid navigation map is formed by the longitude route and the latitude route of the embodiment viewed in the overlooking direction, the side length of 4 sides of the grid is 5-15 kilometers, and each side is marked with a heading; the grid is also provided with a net hole 1, a net hole 2 and a net hole 3, and permanent and temporary flight forbidding areas such as a flight forbidding area, a flight obstacle area, a free flight area, a national major engineering area, a temporary control area and the like can be arranged in the net hole; left-handed dual independent take-off and landing disk airports A, B, C and D are provided. A plurality of routes are available for selection when the airport A takes off to land at the airport B, one route is shown in figure 2, the left-handed disk takes off from the airport A and ascends to enter a weft route w2, the east-handed disk flies to a warp route j12, the north-handed disk rotates 90 degrees upwards to cut into the warp route j12 and flies to the weft route w8 to land at the airport B, and the left-handed disk lands at the airport B after landing; similarly, when the aircraft flies from an airport B to an airport C, a plurality of flight paths can be selected, one of the flight paths is shown in FIG. 2, the aircraft flies from the airport B and rises left-handed disk to enter a weft flight path w8, flies eastward to a warp flight path j13, flies upwards 90 degrees to south, cuts into a warp flight path j13 to fly to the weft flight path w5 and arrives at the airport C, and the aircraft lands at the airport C after the left-handed disk descends; similarly, when the aircraft flies from the airport C to the left-handed airport D, a plurality of routes can be selected, one route is shown in figure 2, the aircraft flies from the airport C, flies left-handed and rises to enter a weft route w5, flies west to a warp route j6, turns north to 90 degrees, flies up to a warp route j6, flies to the airport D through a weft line w10, and lands on the airport D after the left-handed disk descends.

In the construction layout of the left-handed airport A, B, C, D, the left-handed meshes of the flight path are selected from the flight path mesh figure 2 at the proposed airport, that is, the heading arrows on the 4 sides of the flight path meshes are all the meshes A, B, C and D which are connected end to end and are left-handed, and the airports are respectively constructed in the selected meshes, so as to realize the safe, efficient, reliable, simple, convenient and autonomous operation of the low-altitude airspace fixed wing aircraft airport.

Example three:

this embodiment is substantially the same as the previous embodiment, and is characterized in that:

in the embodiment, a fixed wing airplane or a self-rotating gyroplane left-handed double independent take-off and landing disk airport is arranged in a grid flight path with weft threads on the upper part and warp threads on the lower part, an airport is built in the center of the airport grid, two landing runways and two take-off runways are respectively and independently separated, a double-isolation flight path design with a landing rectangular flight track and a lifting rectangular flight track which are respectively and independently separated is adopted, the two landing runways and the lifting rectangular flight track are self-formed into an independent subsystem, the two independent subsystems are mutually isolated and do not mutually interfere in operation, an airport terminal building is built in the center of the selected flight path grid, a runway parallel to the weft threads is respectively arranged at a set distance from the terminal building on the south side and the north side of the airport terminal building, the length and the width of the runway are implemented by technical parameters of the largest corresponding type of airplane type of landing model and the design specifications of the current runway, a south side take-off runway is arranged in parallel with the south side landing runway at a distance from the south side landing runway, a north side take-off runway is arranged in parallel with the north side landing runway at a distance from the north side landing runway, the length and width of the runways are implemented by the technical parameters of the largest corresponding type of airplane model for taking off and the design specifications of the current runways, a south side parking apron is arranged between the south side landing runway and the airport terminal building, the airplane can turn to enter the south side parking apron at the end of the landing runway after landing on the south side runway, a north side parking apron is arranged between the north side landing runway and the airport terminal building, the airplane can turn to enter the north side parking apron at the end of the north side runway after landing on the north side runway, the central lines of the south side landing runway and the north side runway simultaneously extend to an east distance grid at the longitude grid, connecting the ends of two central lines, wherein the central lines of a south landing runway and a north landing runway extend to the west at the same time and are away from the meridian of the grid by a set distance, and connecting the ends of the two central lines to form a rectangular landing flight track arranged in the airline grid for the south landing runway and the north landing runway; during taking off, the airplanes of the south side parking apron and the north side parking apron firstly drive into the flying points of the south side flying runway and the north side flying runway of the respective flying runways, the airplanes respectively fly straight to the longitude flight line after taking off and penetrate through the rectangular lifting flight track from the lower part of the longitude flight line, the lifting flight line enters the longitude flight line for flying after reaching the height of the longitude flight line, and then the airplanes respectively lift from the longitude flight line and enter the latitude flight line for flying if necessary. In the selected left-handed flight path grid, a left-handed single independent take-off and landing disk airport is arranged, an airport terminal is built in the center of the selected grid by taking the layout of the left-handed double independent take-off and landing disk airport as a template, only a south landing runway, a south take-off runway and a south parking apron on the south side of the terminal are built or first-stage engineering is built, rectangular landing tracks and rectangular disk lifting tracks are reserved to form a left-handed south independent stand-off aircraft field, or the airport terminal is built in the center of the selected grid, only a north landing runway, a north flying runway and a north parking apron on the north side of the terminal are built or first-stage engineering is built, the rectangular disk lifting tracks and the rectangular disk lifting tracks are reserved to form a left-handed north independent stand-off aircraft field, a double-isolated flight path design that the disk lifting rectangular flight tracks and the disk lifting rectangular flight tracks are respectively and independently separated is formed, so that one runway and the disk lifting rectangular flight tracks are automatically landed to form an independent subsystem, one takeoff runway and the lifting rectangular flight track form another independent subsystem, and the two independent subsystems are isolated from each other and do not interfere with each other in operation.

Example four:

in the embodiment, as shown in fig. 4, a fixed-wing airplane left-handed double independent take-off and landing disc airport is arranged in a flight path grid with warps on the upper portion and wefts on the lower portion to form a left-handed double independent take-off and landing disc airport layout, a terminal 20 is established in the center of a selected left-handed grid, landing runways parallel to the warps are respectively arranged at positions 500-1000 m away from the terminal 20 on the east side and the west side of the terminal, the length and width of the runways are implemented by technical parameters of the largest fixed-wing airplane type designed to land and current runway design specifications, an east take-off runway 25 is arranged in parallel with the east landing runway 26 at a position 100-300 m away from the east landing runway 26 on the east side of the east landing runway 26, a west take-off runway 21 is arranged in parallel with the west landing runway 22 at a position 100-300 m away from the west landing runway 22 on the west side of the west landing runway 22, and the length and width of the runways are implemented by technical parameters of the largest fixed-wing airplane type designed to take-off and the current design The standard implementation is that an east parking apron 24 is arranged between an east landing runway 26 and a terminal building 20, after the airplane descends on the east landing runway 26, the airplane turns to the east parking apron 24 at the end of the landing runway, a west parking apron 23 is arranged between the west landing runway 22 and the terminal building 20, after the airplane descends on the west landing runway 22, the airplane turns to the west parking apron 23 at the end of the west landing runway 22; two end parts of two central lines are respectively formed at the positions of 500-1000 meters away from the latitude line routes 29 and 31, which extend to the south and the north simultaneously from the central lines of the east landing runway 26 and the west landing runway 22, the routes of the two central lines are respectively connected with the north end and the south end of the east landing runway 26 and the north end and the south end of the west landing runway 22, the routes parallel to the latitude line routes 29 and 31 are respectively connected with the north end and the south end of the two central lines to form a rectangular landing flight track 27 which is shared by the east landing runway and the west landing runway, when an airplane lands, the airplane flying on the latitude line routes 29 and 31 can directly cut into the landing flight track 27, the airplane flying on the longitude line routes 30 and 32 firstly descends to the latitude lines 31 and 29 and then cuts into the landing flight track 27 of the landing line, the latitude line routes 29 and 31 and the longitude line routes 30 and 32 form 4 sides of a grid line, the landing flight track is arranged at the outer side of the 4 sides of the grid line, and the landing track is formed at, 4 corners of the outer side flight path are in transitional connection in the form of circular arcs to form a disc-lifting flight track 28 for the eastern flying runway 25 and the western takeoff runway 21 to share; during taking off, the airplanes of the east parking apron 24 and the west parking apron 23 firstly drive into the take-off points of the east take-off runway 25 and the west take-off runway 21 which respectively correspond to the east take-off runway, after taking off, the airplanes respectively fly straight weft line 29 and 31 and penetrate through the cut rectangular lifting flight track 28 from the lower part of the straight weft line 29 and 31, and after lifting to reach the height of the weft line, the airplanes enter the weft line 29 and 31 to fly; alternatively, the lines are individually wound up from the weft lines 29, 31 into the warp lines 30, 32 for flight.

Or as shown in fig. 5 and 6, a fixed-wing airplane left-handed single independent take-off and landing disk airport field is set, a terminal 20 is built in the center of a selected left-handed grid by taking a layout of the left-handed double independent take-off and landing disk airport field as a template, an airport terminal 20 is built in the center of the selected left-handed grid, only an east landing runway 26, an east landing runway 25 and an east parking apron 24 on the east side of the terminal are built in the first project or the first project, a rectangular landing runway 27 and a rectangular landing runway 28 are reserved to form the left-handed single independent take-off and landing disk airport field shown in fig. 5, or the terminal 20 is built in the center of the selected grid, only a west landing runway 22, a west landing runway 21 and a west landing runway 21 on the west side of the first project are built in the west side of the first project, The west apron 23, which retains the rectangular plate-down track 27 and the rectangular plate-up track 28, constitutes the left-handed west-style independent take-off and landing disc airport shown in fig. 6.

On the electronic map of general aircraft flight management department and airline company, the longitude and latitude grid navigation map composed of longitude and latitude navigation lines is set up layer by layer according to the requirement of the fixed-wing aircraft of this embodiment, including net hole 1, net hole 2, net hole 3, left-hand airport A, B, C and D, because the path composed of every longitude and latitude navigation line is fixed, all aircrafts are in order flight without mutual interference, the emergency is few in flight, the weather condition can be predicted, the navigation line with bad weather condition can detour, and the dual independent take-off and landing disk airport adopted by this embodiment method has the characteristic of self-discipline operation in most cases except that the special condition needs tower to command, with the help of precise Beidou positioning navigation and high-resolution three-dimensional electronic map or electronic plane map, the whole flight is mainly instrument flight and automatic piloting flight, and is assisted by visual flight; the flight plan from one airport to any airport can realize that a flight user reports to a general aviation management department and an airline company in real time through a navigator, and the management department and the airline company can send alternative air routes to the navigator of the user in real time, so that the system is very efficient and convenient; in the flight process, the general aviation management department and the airline company can also provide services such as flight information, meteorological conditions, prompts, warnings and the like for the pilots; the navigator on the airplane also has the function of transmitting the data of the airplane flight state to the control department in real time, and the system can give out sound and light alarms once abnormal conditions such as boundary-crossing flight, black flight and the like occur, so that the monitoring, the control and the taking of measures are facilitated; after the flight is finished, the related data management departments and the airlines can also be used for post-incident evaluation and punishment and management of illegal and illegal behaviors such as boundary-crossing flight, black flight and the like.

Example five:

this embodiment is substantially the same as the above embodiment, and is characterized in that:

in this embodiment, as shown in fig. 1 and 3, small and medium sized autogyro routes are provided, the cruising floor height of the small and medium sized autogyro is 1450 m above the airspace, the warp routes 14 are laid out, the distance between every two adjacent warps is 1-3 km, and the directions of every two adjacent warp routes are opposite to each other. The height of the lower layer is 1150 meters, the weft air lines 15 are distributed, the interval distance between every two adjacent weft is 1-3 kilometers, and the directions of every two adjacent weft air lines are opposite to each other. As shown in fig. 3, a grid navigation map is formed by the longitude route and the latitude route of the embodiment viewed in the overlooking direction, the side length of 4 sides of the grid is 1-3 kilometers, and each side is marked with a heading; the grid is also provided with a net hole 51, a net hole 52 and a net hole 53, and permanent and temporary flight forbidding areas such as a flight forbidding area, a flight obstacle area, a free flight area, a national major engineering area, a temporary control area and the like can be arranged in the net hole; and the grid navigation chart is provided with a left-handed double independent take-off and landing disk airports E and F. There may be multiple routes from takeoff at airport E to landing at airport F, three of which are shown in fig. 3:

one is as follows: the aircraft takes off from an airport E, flies left and turns up to enter a meridian line jN2, flies north to a latitude line WN10, turns east to 90 degrees, flies down to cut into the latitude line WN10, flies east to enter an airport F through the meridian line jN13, and lands on the airport F after the left-handed disk descends; the second step is as follows: the aircraft flies from an E airport to a left rotary disk, enters a meridian route jN2, flies to a latitude route wN6 in the north direction, turns to the east by 90 degrees, flies downwards to cut into the latitude route wN8, flies to the east to turn to the longitude route jN14 in the north direction by 90 degrees, flies upwards to cut into the longitude route jN14, flies to a latitude route wN10, flies to an airport F, and lands on the airport F after the left rotary disk descends; and thirdly: and (3) taking off from the E airport, lifting the left rotary disk, entering a weft line WN2, flying eastward to a warp line JN14, turning 90 degrees northward, cutting the upward flight into the warp line JN14, flying northward to a weft line WN10, flying to an airport F, and landing the left rotary disk at the airport F.

In the construction layout of the autogyro E, F left-handed airport in the flight path grid with warp lines below the weft lines, the left-handed grid of the flight path is selected at the proposed airport according to the flight path grid graph 3, namely, heading arrows on 4 sides of the flight path grid are all head-to-tail grids E, F with the left-handed direction, and the airport is built in the selected grid, so that safe, efficient, reliable, simple and convenient and autonomous operation of the autogyro airport in the airspace monitoring and airspace reporting is realized. The embodiment is provided with a left-handed double independent take-off and landing disk airport of a self-rotating gyroplane, an airport is built in the center of a left-handed flight path grid, two landing runways and two take-off runways are independently separated, and a disc-lifting rectangular flight track are independently separated to form a double isolation flight path design, as shown in figure 7, the two landing runways and the disc-lifting rectangular flight track form an independent subsystem, the two take-off runways and the disc-lifting rectangular flight track form an independent subsystem, the two independent subsystems are isolated from each other and do not interfere with each other in operation,

as shown in fig. 7, in the flight path grid with the warp lines on the upper side and the weft lines on the lower side, an autorotation gyroplane left-handed double independent take-off and landing disc airport layout is formed, a terminal building 220 is established in the center of the selected left-handed grid, landing runways parallel to the warp lines are respectively arranged at positions 100-300 meters away from the terminal building at the east side and the west side of the terminal building, the length and the width of the runways are executed by the technical parameters of the maximum autorotation gyroplane type designed to land and the design specifications of the existing runways, an east take-off runway 225 is arranged in parallel with the east landing runway 226 at the position 50-100 meters away from the east landing runway 226 at the east side of the east landing runway 226, a west take-off runway 221 is arranged in parallel with the west landing runway 222 at the position 50-100 meters away from the west landing runway 222 at the west side of the west landing runway 222, and a west take-off runway 221 is arranged in parallel with the technical parameters of the maximum autorotation gyroplane type designed and the design specifications An east apron 224 is arranged between the east runway 226 and the station building 220, the aircraft turns to the east apron 224 at the end of the runway after landing on the east runway 226, a west apron 223 is arranged between the west runway 222 and the station building 220, and the aircraft turns to the west apron 223 at the end of the runway 222 after landing on the west runway 222; two ends of two central lines are respectively formed at positions which are 100-300 meters away from the weft line 231 and 229 and extend to the south and the north simultaneously from the central lines of the east landing runway 226 and the west landing runway 222, wherein the two ends comprise the north end and the south end of the east landing runway 226 and the north end and the south end of the west landing runway 222, the routes parallel to the weft line 231 and 229 respectively connect the north end and the south end of the two central lines to form a rectangular landing flight track 227 for the east and west landing runways to share, when the airplane lands, the airplane flying on the weft line 229 and 231 can directly cut into the landing rectangular flight track 227, the airplane flying on the warp line 230 and 232 firstly descends to the weft line 231 and 229 and then cuts into the landing rectangular flight track 227, the weft line 231 and 229 and the warp line 230 and 232 form 4 sides of a grid line, and the landing flight track is arranged outside the 4 sides of the grid line, an outer flight line is formed at a distance of 100-200 meters from a side line of the grid flight line from a flight line, 4 corners of the outer flight line are in transitional connection in a circular arc line form to form a disc-rising rectangular flight track 228 for sharing with an east-rising runway 225 and a west-rising runway 221, during flying, autorotation rotorcraft of the east-landing apron 224 and the west-landing apron 223 firstly drive into respective flying points of the east-landing runway 225 and the west-rising runway 221, after the aircraft takes off, respective straight flying weft line 229 and 231 pass through and are cut into the disc-rising rectangular flight track 228, and after the disc-rising reaches the height of the weft line, the weft line 229 and 231 fly, or respectively rise from the weft line 229 and 231 and enter the warp line 230 and 232;

or, setting a left-handed single independent take-off and landing disk airport of the autorotation rotorcraft, establishing an airport terminal 220 in the center of the selected grid by taking a layout drawing of the left-handed double independent take-off and landing disk airport of the autorotation rotorcraft as a template, only constructing an east landing runway 226, an east landing runway 225 and an east parking apron 224 on the east side of the terminal in the first project or first constructing the first project, and reserving a rectangular disk lifting track 227 and a rectangular disk lifting track 228 to form the left-handed east single independent take-off and landing disk airport of the autorotation rotorcraft; or, an airport terminal 220 is established in the selected grid center, only a west landing runway 222, a west departure runway 221 and a west parking apron 223 on the west side of the terminal are established or first-stage engineering is established, and a rectangular disc lifting track 227 and a rectangular disc lifting track 228 are reserved to form a rotary-wing aircraft levorotation west single independent take-off and landing disc airport.

The general aircraft flies in a monitoring airspace and a reporting airspace according to a fixed longitude and latitude line path, the flying environment from a flying airport to a landing airport and along the periphery of a flight line is predicted, other general aircraft are also predicted when flying in order on the respective longitude and latitude lines of the monitoring airspace and the reporting airspace, a plane electronic terrain landmark map or a three-dimensional ground view electronic map along the flight line is also predicted, and sudden collision events are prevented without being processed and carried out in real time, so that the general aircraft is particularly suitable for instrument flying and automatic driving, and can be realized by depending on a three-dimensional ground view electronic map or an electronic plane map provided by Beidou satellite positioning navigation and high-resolution satellites and an automatic pilot on the general aircraft.

Example six:

in the embodiment, as shown in fig. 8, a fixed-wing airplane left-handed dual independent take-off and landing disk airport is arranged in a flight path grid with weft threads on the upper portion and warp threads on the lower portion, a fixed-wing airplane left-handed dual independent take-off and landing disk airport layout is formed, a terminal building 520 is established in the center of a selected left-handed grid, landing runways parallel to the weft threads are respectively arranged at positions 500-1000 meters away from the terminal building on the south side and the north side of the terminal building, the length and width of the runways are implemented by technical parameters of the largest fixed-wing airplane type designed to land and current runway design specifications, a south take-off runway 525 is arranged in parallel with the south landing runway 526 at a position 100-300 meters away from the south landing runway 526 of the south landing runway 526, a north take-off runway 521 is arranged in parallel with the north landing runway 522 at a position 100-300 meters away from the north landing runway 522 of the north landing runway 522, and a north runway 521 is arranged in parallel with the north runway 522, the length and width of the runway are implemented by technical parameters of the The design specification is implemented, a south parking apron 524 is arranged between the south landing runway 526 and the station building 520, the aircraft turns to the south parking apron 524 at the end of the landing runway after landing on the south landing runway 526, a north parking apron 523 is arranged between the north landing runway 522 and the station building 520, and the aircraft turns to the north parking apron 523 at the end of the north landing runway 522 after landing on the north landing runway 522; two end parts of two central lines are respectively formed at the positions of 500-1000 meters of the central lines of the south landing runway 526 and the north landing runway 522, which simultaneously extend to the east and west directions and have distances of grid meridian 529 and 531, wherein the positions comprise the east end and the west end of the south landing runway 526 and the east end and the west end of the north landing runway 522, the routes parallel to the grid meridian lines 529 and 531 respectively connect the east end and the west end of the two central lines to form a rectangular landing flight track 527 for the south and north landing runways to share, when the airplane lands, the airplane flying on the meridian lines 529 and 532 directly cuts into the landing flight track 527, the airplane flying on the latitude line 530 and the longitude line 531 first descends to the meridian line 531 and 529 and then cuts into the landing flight track 527, the latitude line 530 and 532 and the meridian line 531 and the longitude line 531 and 529 form 4 sides of the grid line, the landing flight track is arranged outside the 4 sides of the grid, an outer route is formed at a position 100-600 meters away from the route from the sideline of the grid route, and 4 corners of the outer route are in transitional connection in the form of circular arcs to form a lifting rectangular flight track 528 for sharing by the south-rising runway 525 and the north-rising runway 521; during taking off, the airplanes of the south parking apron 524 and the north parking apron 523 firstly drive into the take-off points of the south take-off runway 525 and the north take-off runway 521 respectively, after taking off, the airplanes respectively fly straight warp flight routes 529 and 531 and penetrate through a cut-in rectangular lifting flight track 528 from the lower part of the warp flight routes 529 and 531, and after reaching the height of the warp, the lifting flies in the warp flight routes 529 and 531; or, the aircraft respectively ascends from the meridian routes 529 and 531 to enter the latitude routes 530 and 532 for flying;

or, in the selected left-handed flight path grid, a fixed-wing aircraft left-handed single independent take-off and landing disk airport field is set, a fixed-wing aircraft left-handed double independent take-off and landing disk airport field layout picture is taken as a template, an airport terminal 520 is established in the center of the selected grid, only a south landing runway 526, a south take-off runway 525 and a south parking apron 524 of the terminal are established or first-stage engineering is firstly established, rectangular landing tracks 527 and rectangular landing tracks 528 are reserved, and the fixed-wing aircraft left-handed south independent take-off and landing disk airport field is formed; or, the airport terminal 520 is built at the selected grid center, only the north landing runway 522, the north flying runway 521 and the north parking apron 523 on the north side of the terminal are built or first-stage projects are built, the rectangular disc landing track 527 and the rectangular disc lifting track 528 are reserved, and the fixed-wing aircraft left-hand and north-hand independent landing disc airport is formed.

In the embodiment, a left-handed double independent take-off and landing disk airport of the fixed-wing aircraft is provided. In the embodiment, the layout of the airport with the fixed-wing aircraft and the left-handed dual independent take-off and landing disks is adopted, the general aircrafts can fly orderly, safely and efficiently on the corresponding longitude and latitude air routes, and the general aviation management department can realize high-quality service, safe, reliable, efficient, simple and convenient flight operation and monitoring management and control.

Example seven:

in the embodiment, as shown in fig. 9, in the flight path grid with the weft threads on the upper part and the warp threads on the lower part, the autorotation gyroplane left-hand double independent take-off and landing disk airport layout is formed, the airport layout with the autorotation gyroplane left-hand double independent take-off and landing disk is established in the center of the selected left-hand grid, the airport 720 is established at the position 100-300 meters away from the airport 720 at the south side and the north side of the airport, a landing runway parallel to the weft threads is respectively arranged, the length and the width of the runway are implemented by the technical parameters of the maximum autorotation gyroplane type designed to land and the design specifications of the existing runway, a south take-off runway 725 is arranged at the position 50-100 meters away from the south landing runway 726 of the south landing runway, a north take-off runway 721 is arranged at the position 50-100 meters away from the north runway 722 of the north runway 726, the length and width of the runway are implemented by technical parameters of a maximum autorotation rotorcraft type for taking off and the design specifications of the existing runway, a south parking apron 724 is arranged between a south landing runway 726 and a station building 720, the aircraft turns to the south parking apron 724 at the end of the landing runway after landing on the south landing runway 726, a north parking apron 723 is arranged between the north landing runway 722 and the station building 720, and the aircraft turns to the north parking apron 723 at the end of the landing runway 722 after landing on the north landing runway 722; at the positions where the central lines of the south landing runway 726 and the north landing runway 722 simultaneously extend towards the east-west direction by a distance of 100-300 meters from the grid warps 729 and 731, two end parts of two central lines are respectively formed, including the east end and the west end of the south landing runway 726 and the east end and the west end of the north landing runway 722, and the routes of the parallel weft route grid warps 729 and 731 respectively connect the east end and the west end of the two central lines to form a rectangular landing flight track 727 for the south and north landing runways to share, when an airplane lands, the airplane flying on the warp routes 729 and 731 directly cuts into the landing rectangular flight track 727, and when the airplane flying on the weft routes 730 and 732 firstly descends to the warp routes 731 and 729 and then cuts into the landing rectangular flight track 727; the latitude line flight paths 730 and 732 and the longitude line flight paths 731 and 729 form 4 sides of a grid flight path, a spiral-lift flight track is arranged on the outer side of the 4 sides of the grid flight path, an outer flight path is formed at a position which is 100-200 meters away from the side line of the grid flight path from the flight path, 4 corners of the outer flight path are in transitional connection in the form of circular arcs to form a spiral-lift rectangular flight track 728 which is shared by a south-rising flight runway 725 and a north-rising flight runway 721, during taking off, self-rotary wing aircraft of a south parking apron 724 and a north parking apron 723 firstly drive into respective take-off points of the south-take-off runway 725 and the north-rising flight runway 721, respectively directly fly the longitude line flight paths 729 and 731 after the aircraft passes through the spiral-lift rectangular flight track 728 under the self-rotary wing aircraft, and then the spiral-lift flight aircraft enters the longitude line flight paths 72; alternatively, the aircraft flies from the warp lanes 729, 731, respectively, winding up into the weft lanes 730, 732;

or, in the selected left-handed flight path grid, setting a self-rotary-wing aircraft left-handed single independent take-off and landing disk airport, taking a self-rotary-wing aircraft left-handed double independent take-off and landing disk airport layout as a template, establishing an airport terminal 720 in the center of the selected grid, only establishing or first-stage engineering firstly establishing a south landing runway 726, a south take-off runway 725 and a south parking apron 724 on the south side of the terminal, and reserving a rectangular disk landing track 727 and a rectangular disk lifting track 728 to form the self-rotary-wing aircraft left-handed south independent take-off and landing disk airport; or, an airport terminal 720 is established in the selected grid center, only the north landing runway 722, the north departure runway 721 and the north parking apron 723 on the north side of the terminal are established or first-stage projects are firstly established, the rectangular disc-descending track 727 and the rectangular disc-ascending track 728 are reserved, and the gyroplane left-handed north single-rise landing disc airport is formed.

In this embodiment, a left-handed dual independent take-off and landing disk airport is provided for the autogyro. The embodiment adopts the layout of the autogyro left-handed double independent take-off and landing disk airport, so that the general aircrafts can fly orderly, safely and efficiently on corresponding longitude and latitude air routes respectively, and the general aviation management department can realize high-quality service and safe, reliable, efficient, simple and convenient flight operation and monitoring management and control.

Example eight:

in this embodiment, as shown in fig. 1, the helicopter is a helicopter, the upper layer is 2000 meters high, the warp routes 12 are laid out, the distance between every two adjacent warp routes is 0.5-2 kilometers, and the directions of every two adjacent warp routes are opposite to each other. The height of the lower layer is 1750 m, the weft air lines 13 are distributed, the interval distance between every two adjacent weft is 0.5-2 km, and the directions of every two adjacent weft air lines are opposite to each other. When the longitude route 12 and the latitude route 13 of the embodiment are seen in the overlooking direction, a grid navigation chart is formed, the side length of 4 sides of the grid is 0.5-2 kilometers, and each side is marked with a course; the net holes are arranged on the grids, and permanent and temporary flight forbidding areas such as a flight forbidding area, a flight obstacle area, a free flight area, a national major engineering area, a temporary control area and the like can be arranged in the net holes. The airports of the helicopter may be arranged in any of the grids of its grid pattern, with the airport layout being performed according to existing specifications.

Example nine:

in this embodiment, as shown in fig. 1, the electric multi-shaft manned helicopter is an electric multi-shaft manned helicopter, the upper layer is 400 meters high, the warp routes 16 are arranged, the distance between every two adjacent warp routes is 200-600 meters, and the directions of every two adjacent warp routes are opposite to each other. The height of the lower layer is 250 meters, the weft air lines 17 are distributed, the interval distance between every two adjacent wefts is 200-600 meters, and the directions of every two adjacent weft air lines are opposite to each other. When the longitude route 16 and the latitude route 17 of the embodiment are seen in the overlooking direction, a grid navigation chart is formed, the side length of 4 sides of the grid is 200-600 meters, and each side is marked with a course; the mesh is provided with mesh holes, and the mesh holes can be a no-fly zone, a flight obstacle zone, a national major engineering zone and a temporary control zone. The airport of the electric multi-shaft manned helicopter can be arranged in any grid of the grid route, and the airport layout refers to the airport layout of the helicopter.

Example ten:

in this embodiment, as shown in fig. 1, the upper layer of the miniature electric multi-axis helicopter is 150 meters high, the warp routes 18 are arranged, the distance between every two adjacent warp routes is 25 to 50 meters, and the directions of every two adjacent warp routes are opposite to each other. The height of the lower layer is 100 meters, the weft air lines 19 are distributed, the interval distance between every two adjacent wefts is 25-50 meters, and the directions of every two adjacent weft air lines are opposite to each other. When the longitude route 18 and the latitude route 19 of the embodiment are seen in the overlooking direction, a grid navigation chart is formed, the side length of 4 sides of the grid is 25-50 meters, and each side is marked with a course; the mesh is provided with mesh holes, and the mesh holes can be a no-fly zone and a flight obstacle zone. The airport of the miniature electric multi-axis helicopter can be arranged in any grid of the grid route, and the airport layout refers to the airport layout of the helicopter.

Example eleven:

in this embodiment, the grids can be combined, since the earth is a spherical star, the distance between two adjacent meridians is accelerated to decrease with the increase of latitude until all meridians at the north pole and the south pole converge into one point, in this process, every time the distance between the meridians is equal to or less than the minimum interval allowed by the type of airline grid or the minimum allowable latitude edge length, 2 meridians among 3 adjacent grids side by side among 2 adjacent wefts are cancelled, and the 3 grids side by side are combined into 1 grid to maintain the requirement of the grid size.

With the further development of the general aviation industry, the altitude of the low altitude airspace may be further released, and the cruise airspace division of the fixed wing aircraft, the helicopter and the autorotation rotorcraft of the invention is adjusted along with the altitude, but the invention point of the invention is not changed.

The embodiments of the present invention have been described above with reference to the accompanying drawings, but the present invention is not limited to the embodiments described above, and various changes and modifications can be made according to the purpose of the invention, and any changes, modifications, substitutions, combinations or simplifications made according to the spirit and principle of the technical solution of the present invention shall be equivalent substitutions, as long as the purpose of the present invention is met, and the present invention shall fall within the protection scope of the present invention as long as the technical principle and inventive concept of the general method for constructing and operating a longitude and latitude wire network of an aircraft are not departed from the present invention.

Claims

1. A method for constructing and operating and controlling a universal longitude and latitude navigation network of an aircraft is characterized by comprising the following steps: according to a fixed wing airplane, a helicopter, a self-rotating gyroplane, an electric multi-shaft manned helicopter or a miniature electric multi-shaft unmanned aerial vehicle, a monitoring airspace and a reporting airspace of 0-3000 m of the true height of the airplane are divided into 5 cruise layer height airspaces; the cruise level airspace of the same type of general aircraft is divided into an upper layer and a lower layer; the upper layer layout of the same cruise floor high airspace is provided with warp routes at intervals, and the lower layer layout of the same cruise floor high airspace is provided with weft routes at intervals; or the upper layer layout of the same cruise layer high airspace sets weft routes at intervals, and the lower layer layout of the same cruise layer high airspace sets warp routes at intervals; defining a series of meridians in the monitoring airspace and the reporting airspace as flight paths of the aircraft from north to south or from south to north; and demarcating a series of wefts to be used as flight routes of the aircraft from east to west or west to east; the course of the adjacent meridian route and the course of the adjacent latitude route of the cruising level airspace of the same type of general aircraft are opposite to each other; 5 air line grid diagrams consisting of a series of meridian route and a series of latitude route are formed in a monitored airspace and a reported airspace, the side line of each grid is a route marked with a single course and a single height, and each grid is defined to be approximately square or rectangular; and each graph is provided with a no-fly net hole and an airport airspace, so that a general aviation monitoring airspace and a report airspace longitude and latitude navigation network are constructed;

2. The method for managing and controlling construction and operation of a universal aircraft transit network according to claim 1, wherein: in the grid route with warp lines on the top and weft lines on the bottom, a left-handed double independent take-off and landing disk airport of a fixed wing aircraft or a self-rotating gyroplane is arranged, an airport is built in the center of the airport grid, two landing runways and two take-off runways are independently separated, a double-isolation route design with a landing rectangular flight track and a lifting rectangular flight track which are independently separated is adopted, the two landing runways and the lifting rectangular flight track are self-formed into an independent subsystem, the two independent subsystems are mutually isolated and do not mutually interfere in operation, an airport terminal building is built in the center of the selected route grid, a landing parallel to the warp lines is respectively arranged at the set distance from the airport terminal building on the east side and the west side, the length and the width of the runway are implemented by the technical parameters of the largest airplane type of the designed landing and the design specifications of the existing runway, an east take-off runway is arranged in parallel with the east landing runway at a set distance from the east landing runway on the east landing runway, a west take-off runway is arranged in parallel with the west landing runway at a set distance from the west landing runway on the west landing runway, the length and width of the runways are implemented by technical parameters of the largest corresponding type of airplane model for taking off and design specifications of the existing runways, an east parking apron is arranged between the east landing runway and an airport terminal building, the airplane can turn to enter the east parking apron at the end of the landing runway after landing on the east landing runway, a west parking apron is arranged between the west landing runway and the airport terminal building, the airplane can turn to enter the west landing apron at the end of the west landing runway after landing on the west landing runway, and the central lines of the east landing runway and west landing runways extend to the north and set distances from grids, connecting the ends of two central lines, wherein the central lines of an east landing runway and a west landing runway simultaneously extend to the south to a set distance from a grid latitude line, and connecting the ends of the two central lines to form a rectangular landing flight track arranged in a route grid and can be shared by the east landing runway and the west landing runway; during taking off, the airplanes of the east-side parking apron and the west-side parking apron firstly drive into the take-off points of the east-side take-off runway and the west-side take-off runway of the respective take-off runways, the respective airplanes directly fly the weft flight lines after taking off and penetrate through the rectangular lifting flight tracks from the lower parts of the weft flight lines, the weft flight lines enter the weft flight lines for flying after the lifting reaches the height of the weft, and the airplanes respectively lift the weft flight lines and fly by the warp flight lines if necessary; in the selected left-handed flight path grid, a left-handed single independent take-off and landing disk airport is arranged, an airport terminal is built in the center of the selected grid by taking the layout of the left-handed double independent take-off and landing disk airport as a template, only an east landing runway, an east take-off runway and an east parking apron on the east side of the terminal are built or first-stage engineering is built, rectangular landing tracks and rectangular disk lifting tracks are reserved to form the left-handed east single independent take-off and landing disk airport, or the airport terminal is built in the center of the selected grid, only a west landing runway, a west landing runway and a west parking apron on the west side of the terminal are built or first-stage engineering is built, the rectangular disk lifting tracks and the rectangular disk lifting tracks are reserved to form the left-handed west single independent take-off and landing disk airport, a double-isolation flight path design that the disk lifting rectangular flight tracks and the disk lifting rectangular flight tracks are respectively and independently separated is formed, so that one rectangular landing runway and the disk lifting rectangular flight tracks form an independent subsystem, one takeoff runway and the lifting rectangular flight track form another independent subsystem, and the two independent subsystems are isolated from each other and do not interfere with each other in operation.

3. The method for managing and controlling construction and operation of a universal aircraft transit network according to claim 1, wherein: in the grid route with weft threads on the upper portion and the lower portion, a left-handed double independent take-off and landing disk airport of a fixed-wing aircraft or a self-rotating gyroplane is arranged, an airport is built in the center of the airport grid, two landing runways and two take-off runways are independently separated, a double-isolation route design with a landing rectangular flight track and a lifting rectangular flight track which are independently separated is adopted, the two landing runways and the lifting rectangular flight track are self-formed into an independent subsystem, the two independent subsystems are mutually isolated and do not mutually interfere in operation, an airport terminal building is built in the center of the selected route grid, a landing parallel to the weft threads is respectively arranged at a set distance from the terminal building on the south side and the north side of the airport terminal building, the length and the width of the runways are implemented by technical parameters of the largest airplane type of the corresponding to the designed landing and the design specifications of the existing runway, a south side take-off runway is arranged in parallel with the south side landing runway at a distance from the south side landing runway, a north side take-off runway is arranged in parallel with the north side landing runway at a distance from the north side landing runway, the length and width of the runways are implemented by the technical parameters of the largest corresponding type of airplane model for taking off and the design specifications of the current runways, a south side parking apron is arranged between the south side landing runway and the airport terminal building, the airplane can turn to enter the south side parking apron at the end of the landing runway after landing on the south side runway, a north side parking apron is arranged between the north side landing runway and the airport terminal building, the airplane can turn to enter the north side parking apron at the end of the north side runway after landing on the north side runway, the central lines of the south side landing runway and the north side runway simultaneously extend to an east distance grid at the longitude grid, connecting the ends of two central lines, wherein the central lines of a south landing runway and a north landing runway extend to the west at the same time and are away from the meridian of the grid by a set distance, and connecting the ends of the two central lines to form a rectangular landing flight track arranged in the airline grid for the south landing runway and the north landing runway; during taking off, the airplanes of the south side parking apron and the north side parking apron firstly drive into the flying points of the south side flying runway and the north side flying runway of the respective flying runways, the airplanes respectively fly straight to the longitude flight line after taking off and penetrate through the rectangular lifting flight track from the lower part of the longitude flight line, the lifting flight line enters the longitude flight line for flying after reaching the height of the longitude flight line, and then the airplanes respectively lift from the longitude flight line and enter the latitude flight line for flying if necessary. In the selected left-handed flight path grid, a left-handed single independent take-off and landing disk airport is arranged, an airport terminal is built in the center of the selected grid by taking the layout of the left-handed double independent take-off and landing disk airport as a template, only a south landing runway, a south take-off runway and a south parking apron on the south side of the terminal are built or first-stage engineering is built, rectangular landing tracks and rectangular disk lifting tracks are reserved to form a left-handed south independent stand-off aircraft field, or the airport terminal is built in the center of the selected grid, only a north landing runway, a north flying runway and a north parking apron on the north side of the terminal are built or first-stage engineering is built, the rectangular disk lifting tracks and the rectangular disk lifting tracks are reserved to form a left-handed north independent stand-off aircraft field, a double-isolated flight path design that the disk lifting rectangular flight tracks and the disk lifting rectangular flight tracks are respectively and independently separated is formed, so that one runway and the disk lifting rectangular flight tracks are automatically landed to form an independent subsystem, one takeoff runway and the lifting rectangular flight track form another independent subsystem, and the two independent subsystems are isolated from each other and do not interfere with each other in operation.

4. The method for managing and controlling construction and operation of a universal aircraft transit network according to claim 2, wherein: in a flight path grid with warps on the upper side and wefts on the lower side, a fixed wing airplane left-handed double independent take-off and landing disc airport layout is arranged, a station building (20) is established in the center of the selected left-handed grid, landing runways parallel to the warps are respectively arranged at the positions 500-1000 m away from the station building (20) on the east side and the west side of the station building, the length and the width of the runways are implemented by technical parameters of the largest fixed wing airplane type for landing design and the design specifications of the existing runways, an east take-off runway (25) is arranged in parallel with the east landing runway (26) at the position 100-300 m away from the east landing runway (26) on the east side of the east landing runway (26), a west take-off runway (21) is arranged in parallel with the west landing runway (22) at the position 100-300 m away from the west landing runway (22) on the west side of the west landing runway (22), the length and the width of the runway are implemented by technical parameters of a maximum fixed wing aircraft model for taking off and the design specification of the current runway, an east parking apron (24) is arranged between the east landing runway (26) and the station building (20), after the aircraft lands on the east landing runway (26), the aircraft turns to enter the east parking apron (24) at the end of the landing runway, a west parking apron (23) is arranged between the west landing runway (22) and the station building (20), after the aircraft lands on the west landing runway (22), the aircraft turns to enter the west parking apron (23) at the end of the west landing runway (22); two end parts of two central lines are respectively formed at the positions 500-1000 meters away from the weft line routes (29, 31) at which the central lines of the east landing runway (26) and the west landing runway (22) simultaneously extend to the south and the north, wherein the two end parts comprise the north end and the south end of the east landing runway (26) and the north end and the south end of the west landing runway (22), the routes parallel to the weft line routes (29, 31) respectively connect the north end and the south end of the two central lines to form a rectangular landing flight track (27) for the east and west landing runways to share, when an airplane lands, the airplane flying on the weft line routes (29, 31) can directly cut into the landing flight track (27), the airplane flying on the warp line routes (30, 32) firstly descends to the weft line routes (31, 29) and then cuts into the landing flight track (27), and the weft line routes (29, 31) and the warp line routes (30, 32) form grid line 4 sides, the spiral-lift flight track is arranged on the outer side of 4 edges of the grid route, an outer route is formed at a position which is 100-600 meters away from the route from the side line of the grid route, and 4 corners of the outer route are in transitional connection in the form of circular arcs to form a spiral-lift flight track (28) which is shared by an east take-off runway (25) and a west takeoff runway (21); during taking off, the airplanes of the east parking apron (24) and the west parking apron (23) firstly drive into the take-off points of the east take-off runway (25) and the west take-off runway (21) which respectively correspond to the east take-off runway, after taking off, the airplanes respectively fly straight weft line (29, 31) and penetrate through the cut rectangular lifting flight track (28) from the lower part of the straight weft line, and after lifting to reach the height of the weft line, the airplanes enter the weft line (29, 31) to fly; or, the aircraft respectively ascends from the latitude line routes (29, 31) to enter the longitude line routes (30, 32) for flying;

or, a fixed-wing airplane left-handed single independent take-off and landing disk airport is set, a terminal building (20) is built in the center of a selected left-handed grid by taking a layout drawing of the left-handed double independent take-off and landing disk airport as a template, an airport terminal building (20) is built in the center of the selected left-handed flight path grid, only an east landing runway (26), an east take-off runway (25) and an east parking apron (24) on the east side of the terminal building are built or first-stage engineering is built, rectangular landing tracks (27) and rectangular disc lifting tracks (28) are reserved to form the left-handed east single independent take-off and landing disk airport, or the terminal building (20) is built in the center of the selected grid, only a west landing runway (22), a west landing runway (21) and a west landing runway (21) on the west side of the terminal building or first-stage engineering is built, The west parking apron (23) is reserved with a rectangular disc-landing track (27) and a rectangular disc-lifting track (28) to form a left-handed west-style independent take-off and landing disc airport.

5. The method for managing and controlling construction and operation of a universal aircraft transit network according to claim 2, wherein: arranging autorotation gyroplane left-handed double independent take-off and landing disc airports in the course grids with the warps on the upper side and the wefts on the lower side to form autorotation gyroplane left-handed double independent take-off and landing disc airport layout, establishing a terminal building (220) in the center of the selected left-handed grid, arranging a landing runway (225) in parallel with the warps at the positions 100-300 meters away from the terminal building on the east side and the west side of the terminal building respectively, setting an east take-off runway (225) in parallel with the east landing runway (226) at the positions 50-100 meters away from the east landing runway (226) on the east side of the east landing runway (226), setting a west take-off runway (221) in parallel with the west landing runway (222) at the positions 50-100 meters away from the west landing runway (222) on the west side of the west landing runway (222), the length and the width of the runway are implemented by technical parameters of a maximum autorotation rotorcraft type for designing take-off and the design specifications of the current runway, an east apron (224) is arranged between an east landing runway (226) and a station building (220), after the aircraft lands on the east landing runway (226), the aircraft turns at the end of the landing runway to enter the east apron (224), a west apron (223) is arranged between the west landing runway (222) and the station building (220), after the aircraft lands on the west landing runway (222), the aircraft turns at the end of the landing runway (222) to enter the west apron (223); two ends of two central lines are respectively formed at positions 100-300 meters away from the weft line routes (231, 229) at which the central lines of the east landing runway (226) and the west landing runway (222) simultaneously extend to the south and the north, wherein the two ends comprise the north end and the south end of the east landing runway (226) and the north end and the south end of the west landing runway (222), the routes parallel to the weft line routes (231, 229) respectively connect the north end and the south end of the two central lines to form a rectangular landing track (227) for the east and west landing runways to share, when an airplane lands, the airplane flying on the weft line routes (229, 231) can directly cut into the landing rectangular flight track (227), the airplane flying on the warp line routes (230, 232) firstly descends to the weft line routes (231, 229) and then cuts into the landing rectangular flight track (227), the weft line routes (231, 229) and the warp line (230, 232) form the edges of a grid flight line 4, the spiral-lift flight orbit is arranged on the outer side of 4 edges of the grid flight path, an outer flight path is formed at a distance of 100-200 meters from the flight path to the side line of the grid flight path, 4 corners of the outer flight path are in transitional connection in the form of circular arcs to form a spiral-lift rectangular flight orbit (228) and are shared by an east take-off runway (225) and a west take-off runway (221), during take-off, autorotation rotorcraft of the east parking apron (224) and the west parking apron (223) firstly drive into the flying points of the east take-off runway (225) and the west take-off runway (221) which respectively correspond to each other, after the aircraft takes off, respective straight flying weft flight paths (229 and 231) penetrate through and are cut into the spiral-lift rectangular flight orbit (228), and then the spiral-lift flight paths (229 and 231) fly after reaching the height of the weft, or respectively spiral-lift flying paths (229 and 231) and enter warp lines (230 and 232) to fly;

or, setting a left-handed single independent take-off and landing disk airport of the autorotation rotorcraft, establishing an airport terminal (220) at the center of a selected grid by taking a layout drawing of the left-handed double independent take-off and landing disk airport of the autorotation rotorcraft as a template, only constructing or first constructing an east landing runway (226), an east landing runway (225) and an east parking apron (224) at the east side of the terminal, and reserving a rectangular disk lifting track (227) and a rectangular disk lifting track (228) to form the left-handed east single independent take-off and landing disk airport of the autorotation rotorcraft; or an airport terminal building (220) is built at the selected grid center, only a west landing runway (222), a west departure runway (221) and a west parking apron (223) on the west side of the terminal building are built or first-stage engineering is built, and a rectangular disc lifting track (227) and a rectangular disc lifting track (228) are reserved to form a left-handed western-style independent take-off and landing disc airport of the autogyro.

6. The method for managing and controlling construction and operation of a universal aircraft transit network according to claim 3, wherein: arranging a left-handed double independent take-off and landing disk airport of a fixed-wing airplane in a flight path grid with weft threads above and warp threads below to form a left-handed double independent take-off and landing disk airport layout of the fixed-wing airplane, establishing a station building (520) in the center of a selected left-handed grid, arranging landing runways parallel to the weft threads at positions 500-1000 meters away from the station building on the south side and the north side of the station building respectively, wherein the length and the width of the runways are implemented by technical parameters of the maximum fixed-wing airplane type for landing and the design specifications of the existing runways, arranging a south take-off runway (525) parallel to the south landing runway (526) at a position 100-300 meters away from the south landing runway (526) on the south side of the south landing runway (526), arranging a north take-off runway (521) parallel to the south landing runway (526) at a position 100-300 meters away from the north landing runway (522) on the north side of the north landing (522), the length and the width of the runway are implemented by technical parameters of a maximum fixed wing airplane type for taking off and the design specifications of the existing runway, a south parking apron (524) is arranged between the south landing runway (526) and the station building (520), the airplane turns to the south parking apron (524) at the end of the landing runway after landing on the south landing runway (526), a north parking apron (523) is arranged between the north landing runway (522) and the station building (520), the airplane turns to the north parking apron (523) at the end of the north landing runway (522) after landing on the north landing runway (522); two ends of two central lines are respectively formed at positions 500-1000 meters away from grid warps 529 and 531 of a south landing runway 526 and a north landing runway 522 in the east-west direction, wherein the positions comprise the east end and the west end of the south landing runway 526 and the east end and the west end of the north landing runway 522, the east end and the west end of the two central lines are respectively connected by routes parallel to the grid warps 529 and 531 of the weft route routes to form a rectangular landing flight track 527 shared by the south and north landing runways, when an airplane lands, the airplane flying on the route 529 and 531 directly cuts into the landing flight track 527, the airplane flying on the weft route 530 and 532 firstly descends to the route warps 529 and then cuts into the landing flight track 527, the weft route 530, 532 and the grid routes 531 and the warps 531 and 529 form a grid route 4, the spiral-lift flight track is arranged on the outer side of 4 edges of the grid route, an outer route is formed at a position which is 100-600 meters away from the route from the side line of the grid route, and 4 corners of the outer route are in transitional connection in the form of circular arcs to form a spiral-lift rectangular flight track (528) which is shared by a south takeoff runway (525) and a north takeoff runway (521); during taking off, airplanes of the south parking apron (524) and the north parking apron (523) firstly run into respective take-off runways of a south take-off runway (525) and a north take-off runway (521) at take-off points, the airplanes respectively fly straight through meridian lines (529 and 531) after taking off and penetrate through a cut rectangular disc-lift flight track (528) from the lower part of the meridian lines, and enter the meridian lines (529 and 531) for flying after reaching the height of the meridian lines; or, respectively winding up from the meridian routes (529, 531) to enter the latitude routes (530, 532) for flying;

or, in the selected left-handed flight path grid, a fixed-wing aircraft left-handed single independent take-off and landing disk airport field is set, a fixed-wing aircraft left-handed double independent take-off and landing disk airport field layout drawing is used as a template, an airport terminal (520) is established in the center of the selected grid, a south landing runway (526), a south landing runway (525) and a south parking apron (524) on the south side of the terminal are only established or first-stage engineering is firstly established, rectangular landing tracks (527) and rectangular lifting tracks (528) are reserved, and the fixed-wing aircraft left-handed south independent take-off and landing disk airport field is formed; or an airport terminal building (520) is built in the selected grid center, only a north landing runway (522), a north flying runway (521) and a north parking apron (523) on the north side of the terminal building are built or first-stage engineering is built, a rectangular disc landing track (527) and a rectangular disc lifting track (528) are reserved, and a fixed-wing airplane left-hand and north independent landing disc airport is formed.

7. The method for managing and controlling construction and operation of a universal aircraft transit network according to claim 3, wherein: arranging autorotation rotorcraft left-handed double independent take-off and landing disk airports in airline grids with weft threads above and warp threads below to form autorotation rotorcraft left-handed double independent take-off and landing disk airport layouts, establishing a terminal building (720) in the center of a selected left-handed grid, setting a landing runway parallel to the weft threads at the position of 100-300 meters away from the terminal building (720) on the south side and the north side of the terminal building respectively, setting a south take-off runway (725) parallel to the landing runway (726) at the position of 50-100 meters away from the south landing runway (726) on the south side of the south landing runway (726), setting a north take-off runway (721) parallel to the north landing runway (722) at the position of 50-100 meters away from the north runway (722) on the north side of the north runway (726), the length and width of the runway are implemented by technical parameters of a maximum autorotation rotorcraft type for taking off and the design specifications of the current runway, a south parking apron (724) is arranged between a south landing runway (726) and a station building (720), the aircraft turns to the south parking apron (724) at the end of the landing runway after landing on the south landing runway (726), a north parking apron (723) is arranged between the north landing runway (722) and the station building (720), the aircraft turns to the north parking apron (723) at the end of the landing runway (722) after landing on the north landing runway (722); at the positions of the south landing runway (726) and the north landing runway (722) where the central lines simultaneously extend to the east and west directions and the distance grid warps (729 and 731) are 100-300 meters, two end parts of two central lines are respectively formed, wherein the two end parts comprise the east end and the west end of the south landing runway (726) and the east end and the west end of the north landing runway (722), the east end and the west end of the two central lines are respectively connected by a route parallel to the weft line course grid warps (729 and 731), so that a rectangular landing flight track (727) is formed and is shared by the south and north landing runways, when an airplane flying on the warp line (729 and 731) directly cuts into the landing rectangular flight track (727), and when the airplane flying on the weft line (730 and 732) firstly descends to the warp line (731 and 729) and then cuts into the landing rectangular flight track (727); the latitude line flight paths (730, 732) and the longitude line flight paths (731, 729) form 4 sides of the grid flight path, the lifting flight track is arranged on the outer side of the 4 sides of the grid flight path, an outer flight path is formed at a position which is 100-200 meters away from the flight path from the sideline of the grid flight path, 4 corners of the outer flight path are in transitional connection in the form of circular arcs to form a lifting rectangular flight track (728) which is shared by a south lifting runway (725) and a north lifting runway (721), during lifting, autorotation rotary-wing aircraft of the south parking apron (724) and the north parking apron (723) firstly drive into respective lifting runway south lifting runway (725) and north lifting runway (721) starting points, respective straight lifting flight paths (729, 731) after the aircraft is lifted and penetrate through the lifting rectangular flight track (728) from the longitude lines, and then the lifting flight paths (729, 731) are lifted and fly after reaching the longitude height; or, flying from the warp lanes (729, 731) individually winding into the weft lanes (730, 732);

or, in the selected left-handed flight path grid, setting a self-rotary-wing aircraft left-handed single independent take-off and landing disk airport, establishing an airport terminal (720) in the center of the selected grid by taking a self-rotary-wing aircraft left-handed double independent take-off and landing disk airport layout as a template, and only constructing or first-stage engineering to firstly construct a south landing runway (726), a south flying runway (725) and a south parking apron (724) on the south side of the terminal, and reserving a rectangular disk landing track (727) and a rectangular disk lifting track (728) to form the self-rotary-wing aircraft left-handed south independent take-off and landing disk airport; or an airport terminal building (720) is built in the selected grid center, only a north landing runway (722), a north flying runway (721) and a north parking apron (723) on the north side of the terminal building are built or first-stage projects are built, and a rectangular disc-descending track (727) and a rectangular disc-ascending track (728) are reserved to form a gyroplane left-handed north single-standing disc-descending airport.

8. The method for managing and controlling construction and operation of the universal longitude and latitude aircraft net according to claims 1-7, characterized in that: in any one grid diagram of 5 airline grid diagrams corresponding to 5 types of general aircrafts, controlled airspace, national major engineering area, flight obstacle area, tourist attraction area, free flight area, temporary no-fly area, permanent and temporary no-fly airspace are in the isolated net hole where flying in and flying over are forbidden; the controlled airspace comprises a military no-fly zone; the national major engineering area comprises areas of nuclear power stations, major hydraulic engineering and large airports; the flight obstacle area comprises high-outburst terrains, ultrahigh buildings, overhead power transmission line towers and areas where wind driven generators are located; the tourist attraction comprises airspace where the scenic attraction is organized such as aircraft flight, fire balloon flight, flight wing flight and unmanned aerial vehicle flight activity; the free flight area is an airspace specially set by general aviation enthusiasts for coach flight, entertainment flight and free dazzling and technical performance; the temporary no-fly area comprises an aviation exhibition flight performance area, a disaster rescue area and an air target ground danger area of military performance.