CN106403973A - Flight plan vertical route programming method and system - Google Patents
Flight plan vertical route programming method and system Download PDFInfo
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- CN106403973A CN106403973A CN201610756548.8A CN201610756548A CN106403973A CN 106403973 A CN106403973 A CN 106403973A CN 201610756548 A CN201610756548 A CN 201610756548A CN 106403973 A CN106403973 A CN 106403973A
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
- G01C21/26—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 specially adapted for navigation in a road network
- G01C21/34—Route searching; Route guidance
- G01C21/3407—Route searching; Route guidance specially adapted for specific applications
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Abstract
The invention relates to a flight plan vertical route programming method and system, and belongs to the technical field of flight management. The method comprises the following steps: carrying out optimal storage on basic flight performance data in each of the flight stage, the climbing stage, the cruise stage, the descending stage and the landing stage of an airplane, published by an airplane developer or a production department in an airborne performance database form; defining and describing the vertical route information in each of the flight stage, the climbing stage, the cruise stage, the descending stage and the landing stage based on the optical storage; and conveniently storing the basic vertical navigation route information in an airborne state, designing a complete military and civilian plan vertical route information structure based on the basic vertical navigation route information in an airborne state, and programming a flow to form a military and civilian flight plan vertical route. The logic relationship among all above information structures is close, no redundancy appears among pieces of information, the information storage amount is small, and the system, can be conveniently stored or unloaded, and can be used for ground or other airborne devices.
Description
Technical field
The invention belongs to flight management technical field is and in particular to the vertical Route planner of a kind of flight plan and be
System.
Background technology
One of important component part of modern flight management system is the vertical air route of flight plan, and flight management system is airborne
The result that the vertical air route of flight plan is formed after mostling come from the vertical routeing of ground flying plan, ground flying plan is hung down
Direct route road is that the vertical air route of flight management system onboard flight plan carries out correct VNAV during VNAV and leads
The original foundation drawn, as shown in Figure 2.
Traditional flight plan vertical routeing process is manual process, can only pass through manually to consult Performance Manual, and
Manually formulated the vertical air route of flight plan, inefficiency, need to consume substantial amounts of artificial energy and time and could plan to fly
Row plans vertical air route.
Next, is in order to meet onboard flight management system Realtime Prediction or modification flight plan vertical air route demand, and
Meet the demand of Performance Prediction, in onboard flight management system and software, original processing method is that directly transplanting ground is big
The flight performance calculation software of type, can cause airborne computer to consume substantial amounts of computing resource, during including taking a large amount of CPU process
Between and take a large amount of internal memories so that fly pipe computer can not or reduce efficiency complete the high task of other priority, such as navigate
Task is it is impossible to meet the requirement of real-time of whole avionics system.
Content of the invention
In order to solve the above problems, the invention provides a kind of vertical Route planner of flight plan and system, in advance
Carry out flight performance data process, generate various database files, by accessing the form of data file and after-treatment data,
To meet the requirement of Realtime Prediction under the vertical routeing of flight management and airborne analysis state.
Present invention firstly provides a kind of vertical Route planner of flight plan, including：
S1, the aerodynamic configuration data obtaining aircraft, the flight in flight course of engine performance data and aircraft
Energy data, and build aerodynamic model data base, engine mockup data base and flight course each stage performance database successively,
Described flight course includes takeoff phase, ramp-up period, cruising phase, decline stage and the landing period of aircraft；
S2, multigroup aircraft flight under some difference engine performance states and under different external environment condition for the acquisition
The fuel consumption of various stages, travel distance and time；
S3, according in step S1 obtain data and real-time external environment condition, using interpolation calculation aircraft flight
The fuel consumption in each stage, travel distance and time, thus build the vertical routeing of flight plan.
Preferably, the order of the vertical routeing of described flight plan is followed successively by：
Select original base, takeoff runway, destination and landing runway, and obtain the external rings of each airport and runway
Environment information；
Takeoff phase air route is determined according to original base and takeoff runway；
Ramp-up period air route is determined according to takeoff phase air route；
Landing period air route is determined according to destination and landing runway；
Decline stage air route is determined according to landing period air route；
Cruising phase air route is determined according to ramp-up period air route and decline stage air route.
In such scheme preferably, described step S1 and step S2 complete in ground loading station, and step S3 flies airborne
Complete in row management system.
Another aspect of the present invention provides a kind of flight plan vertical routeing system, including：
Aerodynamic model data base, for storing the aerodynamic configuration data of aircraft；
Engine mockup data base, for storing engine performance data；
Flight course each stage performance database, for storing flight performance data in flight course for the aircraft, described
Flight course includes takeoff phase, ramp-up period, cruising phase, decline stage and the landing period of aircraft；
Flight plan vertical air route information database, for storing some difference engine performance datas and different outside
The fuel consumption in multigroup aircraft flight each stage under the conditions of environmental data, travel distance and time；
Flight plan vertical routeing module, for vertically navigating according to real-time external environment condition and described flight plan
The information of road information data library storage, calculates fuel consumption, travel distance and the time in aircraft flight each stage, and then plans
The vertical air route of flight plan.
Preferably, described flight plan vertical air route module includes：
Read in unit, the external environment condition for reading original base, takeoff runway, destination and landing runway is believed
Breath；
Takeoff phase air route determining unit, for determining takeoff phase air route according to according to original base and takeoff runway；
Ramp-up period air route determining unit, for determining ramp-up period air route according to takeoff phase air route；
Landing period air route determining unit, for determining landing period air route according to destination and landing runway；
Decline stage air route determining unit, for determining decline stage air route according to landing period air route；
According to ramp-up period air route and decline stage air route, cruising phase air route determining unit, for determining that cruising phase is navigated
Road.
In such scheme preferably, described flight plan vertical air route module is arranged in onboard flight management system,
Can read and identify the flight plan vertical air route information data library file being come by the transmission of ground loading station.
The present invention utilizes the vertical Route planner of the dual-use flight plan in ground and related equipment and system, possesses
Advantages below：1) key property under the related various normal flight conditions of storage flight management and VNAV information；2) deposit
(single double engine failure pattern) performance and VNAV information under the abnormal flying condition of storage；3) quick planning is multigroup military-civil with establishment
The vertical air route of flight plan；4) flexibly change air route vertical with adjusting multigroup military-civil flight plan；5) loaded by ground and set
After standby loading, for onboard flight management system.
Flight plan vertical routeing system is managed by ground flying and facility planning completes complete flight plan and hangs down
Direct route road, forms data file, is blocked by loading, is loaded into onboard flight management system, for execution flight meter in flight course
Draw vertical air route to use.
Brief description
Fig. 1 is that the airborne performance data library structure of flight plan of the present invention vertical routeing system one preferred embodiment shows
It is intended to.
Fig. 2 is that schematic diagram is planned with horizontal path in vertical air route.
Fig. 3 is that the flight management flight plan level vertical RTE DATA table establishment process of embodiment illustrated in fig. 1 of the present invention is shown
It is intended to.
Fig. 4 is that the flight plan vertical RTE DATA file forming process of the planning of embodiment illustrated in fig. 1 of the present invention is illustrated
Figure.
Fig. 5 is airborne performance database Generating Data File, loading and the flight management system of embodiment illustrated in fig. 1 of the present invention
System application process schematic diagram.
Specific embodiment
For making purpose, technical scheme and advantage that the present invention is implemented clearer, below in conjunction with the embodiment of the present invention
Accompanying drawing, the technical scheme in the embodiment of the present invention is further described in more detail.In the accompanying drawings, identical from start to finish or class
As the label element that represents same or similar element or there is same or like function.Described embodiment is the present invention
A part of embodiment, rather than whole embodiments.Embodiment below with reference to Description of Drawings is exemplary it is intended to use
In the explanation present invention, and it is not considered as limiting the invention.Based on the embodiment in the present invention, ordinary skill people
The every other embodiment that member is obtained under the premise of not making creative work, broadly falls into the scope of protection of the invention.Under
Face combines accompanying drawing and embodiments of the invention is described in detail.
In describing the invention it is to be understood that term " " center ", " longitudinal ", " horizontal ", "front", "rear",
The orientation of instruction such as "left", "right", " vertical ", " level ", " top ", " bottom " " interior ", " outward " or position relationship are based on accompanying drawing institute
The orientation showing or position relationship, are for only for ease of the description present invention and simplify description, rather than the dress of instruction or hint indication
Put or element must have specific orientation, with specific azimuth configuration and operation, therefore it is not intended that protecting to the present invention
The restriction of scope.
The invention provides a kind of vertical Route planner of flight plan and system, carry out in advance at flight performance data
Reason, generates various database files, by accessing the form of data file and after-treatment data, vertical to meet flight management
The requirement of Realtime Prediction under routeing and airborne analysis state.
Present invention firstly provides a kind of vertical Route planner of flight plan, including：
S1, the aerodynamic configuration data obtaining aircraft, the flight in flight course of engine performance data and aircraft
Energy data, and build aerodynamic model data base, engine mockup data base and flight course each stage performance database successively,
Described flight course includes takeoff phase, ramp-up period, cruising phase, decline stage and the landing period of aircraft；
S2, multigroup aircraft flight under some difference engine performance states and under different external environment condition for the acquisition
The fuel consumption of various stages, travel distance and time；
S3, according in step S1 obtain data and real-time external environment condition, using interpolation calculation aircraft flight
The fuel consumption in each stage, travel distance and time, thus build the vertical routeing of flight plan.
In step sl, the aerodynamic configuration data, engine performance data and the aircraft that obtain aircraft first were flying
Flight performance data in journey, and build aerodynamic model data base, engine mockup data base and each rank of flight course successively
Section performance database, described flight course include takeoff phase of aircraft, ramp-up period, cruising phase, the decline stage and
The land stage.With reference to three data bases in left side in Fig. 1.
It is understood that Fig. 2 is the overall process schematic diagram that aircraft executes flight, the flight of aircraft has included
Winged stage, ramp-up period, cruising phase, decline stage and landing period, when carrying out routeing design, should be hung down
Direct route circuit planning carry out horizontal path planning again it is illustrated that in, described takeoff phase refers to flying height below 400 feet.
In the present embodiment, the aerodynamic model data base of structure in step S1, mainly by aircrafts such as lift coefficient, resistance pole-faces
The data base of aerodynamic configuration data composition, described engine mockup data base is mainly by motor power model and oil consumption characteristic
The data base of data composition, comprises various thrust modes, thrust restriction, thrust use state data and corresponding oil consumption characteristic quantity
According to.
It is understood that the data in above-mentioned engine mockup data base is mainly used to calculate data below：
1) it is used for data (takeoff phase, maximum continuous ramp-up period, the maximum speed completing to calculate the restriction of each phase thrust
Degree cruising phase).
2) it is used for the data completing RED TO and assuming temperature takeoff phase；
3) related data under air intake duct air door use state；
4) thrust-drag margin setting；
5) relation data between thrust, fuel flow, tremor resistance；
6) thrust arrange parameter (compression ratio or N1 revolution).
Also include in step S1 building flight course each stage performance database, be primarily referred to as taking off/approach is basic
Performance database and airflight performance key property data base.
Wherein, take off/approach key property data base is mainly used in the calculating of data below：
1) complete to calculate the data of V1, VR and V2 speed；It is understood that V1 is the decision speed that takes off, take off
To V1, if single-shot stops, or the situation having other harm flight safeties sliding speedup of running occurs, and should terminate taking off, if table
Speed is more than V1, then in the case of standard runway length, before do not had sufficiently long runway to stop, should continue
Fly；VR is rotation speed, general keeps 10-15 degree to face upward attitude angle；V2 is safe take-off speed, liftoff rear, suitably adjustment
Attitude angle, accelerates to V2 as early as possible, and continues to accelerate to standard climbing speed；
2) approach speed data；
3) climbing speed data.
Airflight performance key property data base is mainly used in the calculating of data below：
1) the main speed plan including flight each stage, altitude information and other performance parameters and performance limit.
2) economy climbing speed data (all power failure states and separate unit failure state)；
3) economy cruising speed data (all power failure states and separate unit failure state)；
4) economy decrease speed data (all power failure states and separate unit failure state)；
5) waft under approach phase speed data；
6) holding patterrn flight speed data；
7) maximum follow-on mission speed data；
8) speed for maximum endurance data (LRC)；
9) maximum angle of climb climbing speed data；
10) MAX CLB climbing speed data；
11) speed under wing flap/slat/undercarriage use state；
12) ceiling altitude (all power failure states and separate unit failure state)；
13) departure time, fuel oil, range data of taking off；
14) go around time, fuel oil, flying distance data；
15) alternate fight plan time, fuel oil, flying distance data；
16) weight data under optimal height/Optimal gradient climbs；
17) relation data between fuel oil and weight.
Step S2, the multigroup aircraft obtaining under some difference engine performance datas and external environment condition data qualification fly
The fuel consumption of row various stages, travel distance and time, with reference to the data base on right side in Fig. 1.Separately below to aircraft once
Five stages of flight are described respectively：
Takeoff phase：According to different thrust modes, climb in different airport pressure altitudes, the temperature difference, gross weight and initially
Under velocity conditions, calculate described takeoff phase flying distance, time and fuel consumption；
Ramp-up period：According to different climb modes, in different airport pressure altitudes, gross weight, indicator air speed/Mach
Under number, temperature difference condition, calculate described ramp-up period flying distance, time and fuel consumption, climb altitude；
Cruising phase：According to different climb modes, at various height, gross weight, indicator air speed/Mach number, temperature difference bar
Under part, calculate described cruising phase fuel flow, away from discrete time；
Decline stage：According to the different drop modes that climbs, at various height, gross weight, indicator air speed/Mach number, temperature
Under the conditions of difference and vertical-path angle (VPA angle), calculate the fuel flow of described decline stage, away from discrete time；
Enter nearly landing period：Under the conditions of airport pressure altitude, gross weight and final decrease speed, enter near described in calculating
Land stage flying distance, time and fuel consumption.
Taking takeoff phase information database as a example, respectively calculate 1000m, 2000m ... 10000m runway distance under, temperature
Difference is 10 DEG C, initial climbing speed is the corresponding departure time/fuel consumption during vx；
Meanwhile, calculate initial climbing speed be respectively vy, vm, vn when, runway distance be 3000m, the temperature difference be 10 DEG C when
The corresponding departure time/fuel consumption；Etc., and takeoff phase information database is formed according to these data.Other stage letters
Breath database sharing principle is identical.
In step S3, obtain in step sl the aerodynamic configuration data of aircraft, engine performance data and aircraft exist
In flight performance data in flight course and step S2 build the fuel consumption in multigroup aircraft flight each stage, advance away from
From and the time (flight plan vertical air route information database) on the basis of, the complete vertical air route in the design vertical air route of flight plan
Message structure, plans dual-use flight management flight plan vertical air route flow process, as shown in figure 3, specific as follows：
1st step, creates VNAV flight course each stage air route table
Including takeoff phase air route table -- original base pressure altitude, gross weight, the temperature difference, initial climbing speed, takeoff phase
Route reform distance, time and fuel consumption, increase VNAV elemental characteristic information, possess sequence, retrieval, increase, insert
Enter (front insert, insert afterwards), delete certain air route function；
Including ramp-up period air route table --- original base pressure altitude, gross weight, the temperature difference, instruction speed/Mach number, climb
Stage Route reform distance, time and fuel consumption, increase VNAV elemental characteristic information, possess sequence, retrieval, increase
Plus, insertion (front insert, insert afterwards), delete certain air route function；
Including cruising phase air route table --- gross weight, the temperature difference, instruction speed/Mach number, cruising phase Route reform distance,
Time and fuel consumption, increase VNAV elemental characteristic information, possess sequence, retrieval, increase, insert (front slotting, insert afterwards),
Delete certain air route function；
Including decline stage air route table --- destination pressure altitude, gross weight, the temperature difference, instruction speed/Mach number, decline
Stage Route reform distance, time and fuel consumption, increase VNAV elemental characteristic information, possess sequence, retrieval, increase
Plus, insertion (front insert, insert afterwards), delete certain air route function；
Including landing period air route table --- destination pressure altitude, gross weight, the temperature difference, instruction speed/Mach number, landing
Stage Route reform distance, time and fuel consumption, increase VNAV elemental characteristic information, possess sequence, retrieval, increase
Plus, insertion (front insert, insert afterwards), delete certain air route function.
Special duty stage air route table can also be included --- airport pressure altitude, gross weight, the temperature difference, instruction speed/Mach
Number, special duty stage Route reform distance, time and fuel consumption, increase VNAV elemental characteristic information, possess row
Sequence, retrieval, increase, insertion (front insert, insert afterwards), delete certain air route function.
Illustrate, in the table of structure, row represents the different task stage, for example first taking ramp-up period air route table as a example
In the business stage, from the second runway of the 3rd runway to the second airport on the first airport, the second task phase, from the first of the second airport
Runway, to the 4th runway on the 5th airport, arranges in the table of structure and represents, the time-to-climb under corresponding task phase, oil consumption rate.
It is understood that being still described to decline stage air route table with above-mentioned task, the decline stage air route of structure
With ramp-up period air route table row, table represents that content is consistent, list is shown as the fall time in corresponding stage, oil consumption rate.Arrange in above-mentioned table
Value calculating process is determined according to step S2 by interpolation method.
2nd step, creates flight plan level vertical air route table, and flight plan vertical routeing order is as follows：Original base-
Takeoff runway-air route-ramp-up period air route-destination-landing runway-landing period air route-decline stage takeoff phase boat
Road-cruising phase air route, finally connects and generates the vertical air route of flight plan level.Specifically：
1) in the table of flight plan vertical air route, from airport list with the runway list associating, select original base, rise
Run fast, destination, landing runway；
2) in the table of flight plan vertical air route, according to original base, takeoff runway, interpolation calculation takeoff phase boat respectively
Road；
3) in the table of flight plan vertical air route, according to takeoff phase air route, interpolation calculation ramp-up period air route respectively；
4) in the table of flight plan vertical air route, according to destination, landing runway, interpolation calculation landing period boat respectively
Road；
5) in the table of flight plan vertical air route, according to landing period air route, interpolation calculation is climbed decline stage boat respectively
Road；
6) in the table of flight plan vertical air route, according to takeoff phase air route, ramp-up period air route, decline stage boat of climbing
Road, landing period air route, interpolation calculation cruising phase air route respectively；
7) in the table of flight plan vertical air route, above each stage vertical air route is connected, forms complete flight meter
Draw vertical air route table, on this basis, increase the editting functions such as interpolation, deletion, change, sequence, retrieval.
8) according to specific tasks demand, according to flight plan vertical air route mark, or original base, takeoff runway, landing
Airport and landing runway, transfer the vertical air route of flight plan of establishment.
According to Fig. 4, Fig. 5, the vertical routeing system work process (ancients of the flight plan in onboard flight management system
With rear military) implementation steps are as follows：
1st step：Run ground flight performance calculation software data file and generate civil onboard performance and vertical waypoint navigation
Data file (txt) --- essential information data；
2nd step：On the basis of airborne civilian vertical waypoint navigation data file, editor is vertical with adding military task respectively
Waypoint navigation information；
3rd step：Takeoff phase demand or function are managed according to military-civil aircraft flight, generates military-civil takeoff phase performance
Information data file；
4th step：Ramp-up period demand or function are managed according to military-civil aircraft flight, generates military-civil ramp-up period performance
Information data file；
5th step：Cruising phase demand or function are managed according to military-civil aircraft flight, generates military-civil ramp-up period performance
Information data file；
6th step：Decline stage demand or function are managed according to military-civil aircraft flight, generates military-civil decline stage performance
Information data file；
7th step：Decline stage demand or function are managed according to military-civil aircraft flight, generates military-civil landing period performance
Information data file；
8th step：Ramp-up period flight plan vertical air route demand or function are managed according to military-civil aircraft flight, generates army
Vertical air route information data file of civilian takeoff phase；
9th step：Ramp-up period flight plan vertical air route demand or function are managed according to military-civil aircraft flight, generates army
Civilian ramp-up period vertical air route information data file；
10th step：Cruising phase flight plan vertical air route demand or function are managed according to military-civil aircraft flight, generates
Military-civil cruising phase vertical air route information data file；
11st step：Decline stage flight plan vertical air route demand or function are managed according to military-civil aircraft flight, generates
Vertical air route information data file of military-civil decline stage；
12nd step：Landing period flight plan vertical air route demand or function are managed according to military-civil aircraft flight, generates
Military-civil landing period vertical air route information data file；
13rd step：Formed according to flight plan vertical air route message structure, generate military-civil flight plan vertical air route letter
Breath data file.
14th step：Data above file is passed to loading card from ground loading station, then is transferred to by loading deck airborne
Equipment.
On the basis of above, plan the vertical air route of military-civil flight plan, comprise generation, interpolation, deletion, change, sequence
And retrieval individual event or the vertical air route of multinomial flight plan, to meet the requirement in the various editor vertical air routes of military-civil flight plan.
Present invention also offers a kind of vertical routeing system of flight plan, including：
Aerodynamic model data base, for storing the aerodynamic configuration data of aircraft；
Engine mockup data base, for storing engine performance data；
Flight course each stage performance database, for storing flight performance data in flight course for the aircraft, described
Flight course includes takeoff phase, ramp-up period, cruising phase, decline stage and the landing period of aircraft；
Flight plan vertical air route information database, for storing some difference engine performance datas and different outside
The fuel consumption in multigroup aircraft flight each stage under the conditions of environmental data, travel distance and time；
Flight plan vertical routeing module, for vertically navigating according to real-time external environment condition and described flight plan
The information of road information data library storage, calculates fuel consumption, travel distance and the time in aircraft flight each stage, and then plans
The vertical air route of flight plan.
Described flight plan vertical air route module includes：
Read in unit, the external environment condition for reading original base, takeoff runway, destination and landing runway is believed
Breath；
Takeoff phase air route determining unit, for determining takeoff phase air route according to according to original base and takeoff runway；
Ramp-up period air route determining unit, for determining ramp-up period air route according to takeoff phase air route；
Landing period air route determining unit, for determining landing period air route according to destination and landing runway；
Decline stage air route determining unit, for determining decline stage air route according to landing period air route；
According to ramp-up period air route and decline stage air route, cruising phase air route determining unit, for determining that cruising phase is navigated
Road.
Described flight plan vertical air route module is arranged in onboard flight management system, can read and identify by ground
The flight plan vertical air route information data library file that loading station transmission comes.
The present invention utilizes the vertical Route planner of the dual-use flight plan in ground and related equipment and system, possesses
Advantages below：1) key property under the related various normal flight conditions of storage flight management and VNAV information；2) deposit
(single double engine failure pattern) performance and VNAV information under the abnormal flying condition of storage；3) quick planning is multigroup military-civil with establishment
The vertical air route of flight plan；4) flexibly change air route vertical with adjusting multigroup military-civil flight plan；5) loaded by ground and set
After standby loading, for onboard flight management system.
Flight plan vertical routeing system is managed by ground flying and facility planning completes complete flight plan and hangs down
Direct route road, forms data file, is blocked by loading, is loaded into onboard flight management system, for execution flight meter in flight course
Draw vertical air route to use.
Last it is to be noted that：Above example only in order to technical scheme to be described, is not intended to limit.To the greatest extent
Pipe has been described in detail to the present invention with reference to the foregoing embodiments, it will be understood by those within the art that：It is still
Technical scheme described in foregoing embodiments can be modified, or wherein some technical characteristics are carried out with equivalent replacing
Change；And these modifications or replacement, do not make the essence of appropriate technical solution depart from the essence of various embodiments of the present invention technical scheme
God and scope.
Claims (6)
1. a kind of vertical Route planner of flight plan is it is characterised in that include：
S1, the aerodynamic configuration data obtaining aircraft, the engine performance data and aircraft flying quality number in flight course
According to, and build aerodynamic model data base, engine mockup data base and flight course each stage performance database successively, described
Flight course includes takeoff phase, ramp-up period, cruising phase, decline stage and the landing period of aircraft；
S2, multigroup aircraft flight under some difference engine performance states and under different external environment condition for the acquisition
The fuel consumption in each stage, travel distance and time；
S3, according in step S1 obtain data and real-time external environment condition, using each rank of interpolation calculation aircraft flight
The fuel consumption of section, travel distance and time, thus build the vertical routeing of flight plan.
2. the vertical Route planner of flight plan as claimed in claim 1 it is characterised in that：Described flight plan is vertically navigated
The order of circuit planning is followed successively by：
Select original base, takeoff runway, destination and landing runway, and obtain the external environment condition letter of each airport and runway
Breath；
Takeoff phase air route is determined according to original base and takeoff runway；
Ramp-up period air route is determined according to takeoff phase air route；
Landing period air route is determined according to destination and landing runway；
Decline stage air route is determined according to landing period air route；
Cruising phase air route is determined according to ramp-up period air route and decline stage air route.
3. the vertical Route planner of flight plan as claimed in claim 1 it is characterised in that：Described step S1 and step S2
On ground, loading station completes, and step S3 completes in onboard flight management system.
4. a kind of vertical routeing system of flight plan is it is characterised in that include：
Aerodynamic model data base, for storing the aerodynamic configuration data of aircraft；
Engine mockup data base, for storing engine performance data；
Flight course each stage performance database, for storing flight performance data in flight course for the aircraft, described flight
Process includes takeoff phase, ramp-up period, cruising phase, decline stage and the landing period of aircraft；
Flight plan vertical air route information database, for storing some difference engine performance datas and different external environment condition
The fuel consumption in multigroup aircraft flight each stage under data qualification, travel distance and time；
Flight plan vertical routeing module, for according to real-time external environment condition and described flight plan vertical air route letter
The information of breath database purchase, calculates fuel consumption, travel distance and the time in aircraft flight each stage, and then plans flight
Plan vertical air route.
5. the vertical routeing system of flight plan as claimed in claim 4 it is characterised in that：Described flight plan is vertically navigated
Road module includes：
Read in unit, for reading the external environmental information of original base, takeoff runway, destination and landing runway；
Takeoff phase air route determining unit, for determining takeoff phase air route according to according to original base and takeoff runway；
Ramp-up period air route determining unit, for determining ramp-up period air route according to takeoff phase air route；
Landing period air route determining unit, for determining landing period air route according to destination and landing runway；
Decline stage air route determining unit, for determining decline stage air route according to landing period air route；
Cruising phase air route determining unit, for determining cruising phase air route according to ramp-up period air route and decline stage air route.
6. the vertical routeing system of flight plan as claimed in claim 4 it is characterised in that：Described flight plan is vertically navigated
Road module is arranged in onboard flight management system, can read and identify that the flight plan come by the transmission of ground loading station is vertical
Air route information data library file.
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| CN201610756548.8A CN106403973A (en) | 2016-08-29 | 2016-08-29 | Flight plan vertical route programming method and system |
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| CN201610756548.8A CN106403973A (en) | 2016-08-29 | 2016-08-29 | Flight plan vertical route programming method and system |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108052116A (en) * | 2017-12-08 | 2018-05-18 | 中国航空工业集团公司西安飞机设计研究所 | The vertical navigation bootmode automatic Verification system and method for flight management system |
| CN108549395A (en) * | 2018-06-19 | 2018-09-18 | 西安特种飞行器工程研究院有限公司 | Underwater unmanned autonomous navigation device navigation control system and method |
| CN108860631A (en) * | 2017-05-10 | 2018-11-23 | 中国航空工业集团公司西安飞行自动控制研究所 | A kind of performance management system based on fixed wing aircraft |
| CN109215396A (en) * | 2017-06-30 | 2019-01-15 | 泰雷兹公司 | Method for determining vertical-path of the aircraft since its current location, associated computer program product and determining system |
| CN109255473A (en) * | 2018-08-21 | 2019-01-22 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | A kind of Route planner based on touch operation |
| CN109684729A (en) * | 2018-12-25 | 2019-04-26 | 中国民用航空飞行学院 | One kind taking off freight weight limit detection system and method, information data processing terminal |
| CN111240361A (en) * | 2020-01-19 | 2020-06-05 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Flight control method, device and equipment based on four-dimensional data and storage medium |
| CN111309723A (en) * | 2019-10-18 | 2020-06-19 | 中国航空工业集团公司西安飞行自动控制研究所 | Fixed wing aircraft-based airborne performance database establishment method |
| CN112362060A (en) * | 2020-08-28 | 2021-02-12 | 中国南方航空股份有限公司 | Civil aviation flight route planning method |
| CN112805221A (en) * | 2018-08-21 | 2021-05-14 | 系统软件企业有限责任公司 | System and method for determining flight phase/motion state of aircraft |
| CN113615672A (en) * | 2021-08-30 | 2021-11-09 | 山东元一动力科技有限公司 | Jet-propelled plant protection atomizing machine |
| CN114326441A (en) * | 2021-12-31 | 2022-04-12 | 北京世冠金洋科技发展有限公司 | Flight control simulation test method and flight control module |
| CN114399925A (en) * | 2022-02-08 | 2022-04-26 | 安胜（天津）飞行模拟系统有限公司 | Design method of flight management system based on eVOTL airplane |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105574626A (en) * | 2014-10-11 | 2016-05-11 | 中国航空工业集团公司西安飞机设计研究所 | Civil-military dual use flight plan planning method |
| CN105701090A (en) * | 2014-10-11 | 2016-06-22 | 中国国际航空股份有限公司 | Simulator for flight management system |
-
2016
- 2016-08-29 CN CN201610756548.8A patent/CN106403973A/en active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105574626A (en) * | 2014-10-11 | 2016-05-11 | 中国航空工业集团公司西安飞机设计研究所 | Civil-military dual use flight plan planning method |
| CN105701090A (en) * | 2014-10-11 | 2016-06-22 | 中国国际航空股份有限公司 | Simulator for flight management system |
Non-Patent Citations (1)
| Title |
|---|
| 钱向农: ""飞行管理系统机载性能数据库应用技术研究"", 《航空工程进展》 * |
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| CN108860631A (en) * | 2017-05-10 | 2018-11-23 | 中国航空工业集团公司西安飞行自动控制研究所 | A kind of performance management system based on fixed wing aircraft |
| CN108860631B (en) * | 2017-05-10 | 2021-11-02 | 中国航空工业集团公司西安飞行自动控制研究所 | Performance management system based on fixed-wing aircraft |
| CN109215396A (en) * | 2017-06-30 | 2019-01-15 | 泰雷兹公司 | Method for determining vertical-path of the aircraft since its current location, associated computer program product and determining system |
| CN108052116B (en) * | 2017-12-08 | 2020-11-06 | 中国航空工业集团公司西安飞机设计研究所 | Automatic verification system and method for vertical navigation guidance mode of flight management system |
| CN108052116A (en) * | 2017-12-08 | 2018-05-18 | 中国航空工业集团公司西安飞机设计研究所 | The vertical navigation bootmode automatic Verification system and method for flight management system |
| CN108549395A (en) * | 2018-06-19 | 2018-09-18 | 西安特种飞行器工程研究院有限公司 | Underwater unmanned autonomous navigation device navigation control system and method |
| CN108549395B (en) * | 2018-06-19 | 2022-01-25 | 西安特种飞行器工程研究院有限公司 | Navigation control system and method for unmanned underwater autonomous vehicle |
| CN109255473A (en) * | 2018-08-21 | 2019-01-22 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | A kind of Route planner based on touch operation |
| CN112805221A (en) * | 2018-08-21 | 2021-05-14 | 系统软件企业有限责任公司 | System and method for determining flight phase/motion state of aircraft |
| CN112805221B (en) * | 2018-08-21 | 2024-02-02 | 系统软件企业有限责任公司 | System and method for determining the flight phase/movement state of an aircraft |
| CN109684729A (en) * | 2018-12-25 | 2019-04-26 | 中国民用航空飞行学院 | One kind taking off freight weight limit detection system and method, information data processing terminal |
| CN111309723A (en) * | 2019-10-18 | 2020-06-19 | 中国航空工业集团公司西安飞行自动控制研究所 | Fixed wing aircraft-based airborne performance database establishment method |
| CN111309723B (en) * | 2019-10-18 | 2023-11-21 | 中国航空工业集团公司西安飞行自动控制研究所 | Airborne performance database building method based on fixed wing aircraft |
| CN111240361A (en) * | 2020-01-19 | 2020-06-05 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Flight control method, device and equipment based on four-dimensional data and storage medium |
| CN112362060A (en) * | 2020-08-28 | 2021-02-12 | 中国南方航空股份有限公司 | Civil aviation flight route planning method |
| CN112362060B (en) * | 2020-08-28 | 2022-08-26 | 中国南方航空股份有限公司 | Civil aviation flight route planning method |
| CN113615672A (en) * | 2021-08-30 | 2021-11-09 | 山东元一动力科技有限公司 | Jet-propelled plant protection atomizing machine |
| CN114326441A (en) * | 2021-12-31 | 2022-04-12 | 北京世冠金洋科技发展有限公司 | Flight control simulation test method and flight control module |
| CN114399925A (en) * | 2022-02-08 | 2022-04-26 | 安胜（天津）飞行模拟系统有限公司 | Design method of flight management system based on eVOTL airplane |
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