CN101403898A - Input method and apparatus for electronic system of civil aircraft control cabin - Google Patents
Input method and apparatus for electronic system of civil aircraft control cabin Download PDFInfo
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Abstract
The invention provides an input method of an electronic system of a civilian airplane cockpit and a device thereof. The device comprises an airplane performance data base and a navigation route data base; a characteristic data base storing takeoff data, climb data, cruise data, descending data, approach data and landing data; a mask data base storing the data of basic characteristic mask set according to the airplane performance, a flight phase mask set according to flight missions and a flight experience mask set according to airways and technical characteristics; and a multifunctional control display unit which is used for carrying out data input and control for an electronic control and management system related to the airplane cockpit according to an interface provided by the mask data base. By studying and presetting a complete set of phase mission data, fight personnel calls and applies the set of data, fundamentally changing the conventional input method that the data must be input word by word or line by line according to the corresponding display position on a screen.
Description
Technical field
The invention belongs to electronic system of civil aircraft control cabin man-machine interface design field, particularly the input method and the system thereof of control of civil aircraft control cabin associated electrical and Management System Data.
Background technology
Nowadays, the operation automation of civil aircraft has become one of typical technology feature, its relevant avionics system is the entry altitude comprehensive state, it mainly is made up of flight management, flight control and thrust management function system etc., can realize from automatic flight management and the guiding task of flying to landing.
By supermatic flying method, guarantee as far as possible dailyly embody designed flight quality in-flight, the fluctuation of peculiar flight departure and flying quality performance when reducing the flight unit and artificially grasping flight, greatly reduce the flight risk, improve flight safety; Moreover, by real-time dynamic calculation and adjustment rationally, aircraft can be flown with economic scene along required track, improve flight production efficiency.
Supermatic flight has also reduced crew's driver behavior technical requirement and long-term accumulation process significantly, for universal civil aircraft, raising air transportation ability, has immeasurable contribution.
Current, the aviation corporate boss will use the technical standard by " Airlines Electronic Engineering Committee " formulation of the US Airways radio subordinate of group, be ARINC600 Series Design basic standard and 700 series of products design specificationss about 50 standards altogether, content comprises technology such as automatic flight management, wireless communication and navigation, flight demonstration, motor power management and system synthesis.
In these functions, flight management is in system's top layer, according to the basic parameter of aircraft and aircrew's input instruction, resource on the comprehensive machine, obtain environmental baseline by sensor, generate rational flight planning thus, then by flight control and thrust management function, vector aircraft is by set mission profile flight automatically.
Owing to have many change factors in the practical flight process, reasons such as weather, air traffic and airport situation for example, flight management system must be supported aircrew's artificial adjustment and operation, in other words, resolve the man-computer relation under " automatically " and the various levels such as " semi-automatic ".
In current avionics system, the driving cabin electronic system architecture comprises aircraft performance database and navigational route database, property database, multi-functional control display unit as shown in Figure 1.The principal mode of man-machine interface is multi-functional control display unit (MCDU), and this is a kind of input display control unit with screen display, numeral and alphabetic keypad and respective keys and knob.Wherein the operation interface of multi-functional control display unit as shown in Figure 2.
According to above-mentioned ARINC technical manual, the main input mode of this MCDU is by set program design, according to the corresponding display position on the screen, carries out line by line word for word input one by one.Therefore the operation pages of a typical control display unit can reach 70 more than the page.Like this, no matter be the operation element amount of daily flight, the still on top of required training time all is quite significant.
Because flight management need also be set according to mission phase, so its mission mode is various, typical Boeing is 25 management modes nearly, and this just causes input operation very consuming time and that needs are very careful in some cases.
In order to solve this contradiction, one group of control panel of design in addition usually, prepare in the property database in Fig. 1 that promptly takeoff data is arranged, the data of climbing, the data of cruising, down drop data, advance nearly data, landing data etc.So that needing the time requirement of manual intervention, for example changing the grade of aircraft.This panel is commonly called the offline mode control panel.
For this reason, Dang Dai avionics system need carefully design and divide these input methods.Usually, by the offline mode control panel can carry out height, course/flight path, highly/setting and the modification of height layer, grade/flight-path angle.And the selection of flight planning, flight performance requirement and economic model generally need be finished by the multi-functional control display device.
This just requires to reach consistent on logic and the algorithm in the design of whole input method.Promptly for the flight unit, this cover input method must be complete, simple, direct and distinct.Do not have between the various selections ambiguity, repeat channel and inharmonic function can correctly use apace under high work load so that guarantee unit.
In order to ensure flight safety, reduce user's training cost, the input method of this system is universalization as far as possible, standardization also.
Sustainable growth along with air traffic, the continuous application of new navigation system technology, the task of flight management becomes increasingly complex, the input method of above-mentioned traditional multi-functional control display unit seems more and more too fat to move, function pages is more and more, is shot through with normal running program, update routine and emergency procedure again.This has just caused its logical relation complexity, and performance history is long, series of malpractice such as cost height; And in practical flight, inefficient operation, loading error takes place frequently.
In the world wide, annual all can have factor to cause the example of aircraft accident according to input error, relates to aircraft and comprise U.S.'s Boeing-747,757,737 aircrafts and European airbus A320, A340 aircraft etc., causes in various degree aircraft damage and casualties.
Raising along with computer process ability, the product platform processing power of avionics system strengthens greatly, can higher processing demands be proposed to system, in addition, the large screen display control technology is becoming the main flow man-machine interface of avionics system, simultaneously, the comprehensive degree of avionics system is more and more higher, use modular open platform to come the synthetic nucleus heart function, how to make full use of the feature of these new technologies and new resources, research and develop new system information input method,, alleviate aircrew's work load to give full play to the comprehensive benefit of these new technologies, improve the visual field of driving cabin, expand the application space of driving cabin, improve comfort level, become the technical matters that this area presses for solution.
Summary of the invention
The object of the present invention is to provide a kind of input method and device thereof of electronic system of civil aircraft control cabin, with the input demand of the avionics system that satisfies high integrityization.The present invention is according to engineering experience with to the gains in depth of comprehension of flight safety technical research, function based on Flame Image Process is covered the plate notion, be about to various aerial missions and be designed to substantially " illiteracy plate ", the aircrew is according to flight planning, the selected plate that covers is also by combination, realize wanting the loaded data task fast, and suitably revise on this basis, therefore logical relation simplifies the operation, increase the convenience and the correctness of data input, reduce the workload of daily flight operation, the mental burden of especially thinking deeply and remembering.
According to above-mentioned inventive concept, the present invention by the following technical solutions:
A kind of input media of electronic system of civil aircraft control cabin comprises:
Aircraft performance database and navigational route database are stored with aeroplane performance data and navigation data;
Property database, be connected with navigational route database with described aircraft performance database, be stored with the takeoff data that generates according to the data of storing in described aircraft performance database and the navigational route database, the data of climbing, the data of cruising, following drop data, advance nearly data, landing data;
Cover the plate database, be connected, be used for obtaining data, be stored with the fundamental characteristics of setting according to aeroplane performance and cover plate from described property database with described property database; The mission phase of setting according to aerial mission covers plate; Flying experience according to course line and technical characterictic setting is covered plate;
The multi-functional control display unit is connected with described illiteracy plate database, is used for according to covering the interface that the plate database provides data input and control being carried out in control of aircraft cockpit associated electrical and management system.
The present invention also provides a kind of input method of electronic system of civil aircraft control cabin, comprises covering the plate database, is stored with the fundamental characteristics of setting according to aeroplane performance and covers plate; The mission phase of setting according to aerial mission covers plate; Flying experience according to course line and technical characterictic setting is covered plate; By covering the illiteracy board interface that the plate database provides, data input and control are carried out in control of aircraft cockpit associated electrical and management system.
Compared with prior art, the present invention is by research and the complete phased mission data of a default cover, the aircrew calls and applies mechanically this sets of data according to task, fundamentally changed to carry out traditional input method of word for word importing one by one line by line according to the corresponding display position on the screen.Solved the shortcoming of multi-functional display control unit tradition input mode, simplification simultaneously because of having reduced the demand of offline mode control panel, further increases driving cabin field of front vision space to the demand of offline mode control panel, help flight safety, improve the driving cabin comfort level.Concrete advantage is as follows:
1, significantly reduces the input page of existing input method, expectation is compared with the mode of the multi-functional display control unit of existing main flow, can reduce by 65% the page, if serve as that compare on the basis promptly with existing 70 pages, estimate no more than 25 of the page of the present invention, therefore can estimate to reduce 65% the page.
2, by covering the input method technology that plate presets, reduce the workload of word for word importing line by line of daily flight, thereby improve operational benefits, reduce the possibility of daily loading error.
3, reduce aircrew's regular job workload, the training of learning and memory thus.Reduce training cost and can improve user's economic benefit, increased the social benefit of airline by improving flight safety.
4, the present invention is that experience is covered customization, the personalization and stylized that plate can be realized identical product as the core of intention.Therefore realize airline's aerial mission characterization easily, have extremely strong course line specific aim and economic confidentiality, thereby improve the core competitiveness of airline flights flight, the economic benefit of fleet scale and the social benefit of full company.
5, the present invention helps to improve the gold content of the intellecture property of avionics system that China develops voluntarily and civil aircraft.
Description of drawings
Fig. 1 is the input media theory diagram of existing electronic system of civil aircraft control cabin;
Key and press-button structure synoptic diagram are Aned in the operation interface of the existing multi-functional control display unit of Fig. 2 and control;
Fig. 3 is the input media theory diagram of electronic system of civil aircraft control cabin of the present invention;
Fig. 4 to Figure 12 is the action pane picture of example of the present invention.
Embodiment
Embodiment one
As shown in Figure 1, a kind of input media of electronic system of civil aircraft control cabin comprises:
Aircraft performance database and navigational route database are stored with aeroplane performance data and navigation data;
Property database, be connected with navigational route database with described aircraft performance database, be stored with the takeoff data that generates according to the data of storing in described aircraft performance database and the navigational route database, the data of climbing, the data of cruising, following drop data, advance nearly data, landing data;
Cover the plate database, be connected, be used for obtaining data, be stored with the fundamental characteristics of setting according to aeroplane performance and cover plate from described property database with described property database; The mission phase of setting according to aerial mission covers plate; Flying experience according to course line and technical characterictic setting is covered plate;
The multi-functional control display unit is connected with described illiteracy plate database, is used for according to covering the interface that the plate database provides data input and control being carried out in control of aircraft cockpit associated electrical and management system.
Wherein, it is to cover plate according to the basis that concrete type designs that described fundamental characteristics covers plate, and purpose is to provide the basic parameter input that aeroplane performance is relevant with the navigation resource easily.The initialization data that this mainly is meant aircraft system comprises aeroplane performance, navigation performance and relevant data configuration, with this as the system start-up and the basis of restarting.
Wherein, it is in conjunction with the type characteristic that described mission phase covers plate, cover plate according to the instrument flight procedure of seaworthiness requirements set, typically comprise prepare, slide, take off, climb, cruise, descend, advance closely before the flight, the stage such as landing, also comprise the necessary modifications stage.All stage design must satisfy sea keeping quality and require and the requirement of instrument flight running program.
Wherein, it is a kind of illiteracy plate of personalization that described flying experience is covered plate, be similar to the individual preference configuration of modern automation control system, feedback data by systems such as flight safety character surveillance system existing in the Civil Aviation System, and summaries such as traffic department, airmanship department, the flight safety department airline operation empirical data concluding out, concrete course line is carried out the function of data preference configuration and cover plate.
Embodiment two
A kind of input method of electronic system of civil aircraft control cabin comprises and covers the plate database, is stored with the fundamental characteristics of setting according to aeroplane performance and covers plate; The mission phase of setting according to aerial mission covers plate; Flying experience according to course line and technical characterictic setting is covered plate; By covering the illiteracy board interface that the plate database provides, data input and control are carried out in control of aircraft cockpit associated electrical and management system.
Wherein, the data of described fundamental characteristics illiteracy plate processing are as follows:
1) aeroplane performance basic parameter input, this comprises the limiting performance of aircraft, for example all kinds of minimum operating speed, maximum flying speed, maximum ceiling, maximum weight and flutter border;
2) initialization data of On-board Navigation resource, for example required coordinate of the initialization of inertial navigation system and course data, magnetic field data, course and RTE DATA, and airport data.
Wherein, described mission phase covers to harden and closes the type characteristic, cover plate according to the instrument flight procedure of seaworthiness requirements set, typically comprise prepare, slide, take off, climb, cruise, descend, advance closely before the flight, the stage such as landing, also can comprise the necessary modifications stage.All stage design must satisfy sea keeping quality and require and the requirement of instrument flight running program.It specifically needs to handle following data:
1) preparatory stage before the flight: initialization action required data, i.e. the master data of this flight:
Take off and weather environment data, load data, fuel oil data, the weight balancing data of landing station;
The navigation resource data that this flight is required;
The instrument program data that this flight is performed;
The ground navigation aid platform data that this flight is performed;
The emergency procedure data that this flight is performed;
The flight plan data that this flight is performed.This comprises performance and parameters such as the necessary input of trajectory predictions calculating gross weight, zero fuel weight, catch fuel oil, cost index and cruising altitude.
In addition,, may need guiding of initialization level and the required related data of vertical guide function, for example need to preset and the corresponding logical condition data that activate according to the functional configuration demand of concrete aircraft system.
2) coast period: this stage is mainly applied mechanically the modification of sliding the mode data, for example the corresponding time that change brought and the fuel consume Data Update of taxiway and runway.
Preset the coasting time and the fuel oil data of corresponding airfield runway;
By recomputating of time and fuel oil data, real-time update flight planning;
The equilibrium point of calculation fuel consume;
According to user's request, can apply mechanically the meteorological condition conversion and cover plate, with update time and fuel oil data.
3) takeoff phase:
The mode of taking off data, this comprises the mode of normally taking off and the derating mode of taking off;
The takeoff data data;
The operation inspection forms data;
The system operation program prompts.
4) ramp-up period:
The mode of climbing data, this comprises economy mode and the single-shot fault mode of climbing of climbing;
The climbing performance data;
The system operation program prompts.
5) cruising phase:
The mode of cruising data mainly comprise all kinds of cruise speed modes and the single-shot mode of cruising;
The wind correction data of cruising;
The system operation program prompts.
6) decline stage:
Decline mode data, this comprises that speed descends and the angle, navigation channel keeps the decline mode;
The descent performance data;
The system operation program prompts.
7) advance the nearly stage:
Advance nearly mode data, this comprises normally advancing near and advancing nearly alter mode;
Advance nearly restricting data;
The system operation program prompts.
8) landing period:
Landing data comprises the control of landing speed and aircraft configuration.
Speed limit data;
The system operation program prompts.
9) modification stage: modification stage is divided into following several option:
Horizontal cross-section is revised data;
Vertical section is revised data.
Wherein, it is for airline provides a cover self-defining illiteracy plate that described flying experience is covered plate, typically comprises course line characteristic, airmanship experience, fuel oil and economic policies and the feature scheme formulated, is exemplified below:
1) the meteorological condition experience is covered plate: be primarily aimed at the feature of local meteorological condition, set company's predetermined process principle, for example plan of being diversion of thunderstorm, boisterous fuel oil back-up plan data.
2) ground queuing is taken off and is waited for and cover plate, is primarily aimed at hub and the amendment scheme set.In existing flight management system, ground characteristics is not considered, yet the ground of current hub waits for that phenomenon is very general, often up to tens of minutes, like this aspect such as fuel oil and weight balancing on the machine need be adjusted and revise, so that carry out the management of fuel oil and weight balancing more accurately.
3) the type take-off and landing characteristic is covered plate, mainly the amendment scheme data of setting according to the concrete feature of aircraft configuration.Nowadays, the aircraft of airline mainly obtains by the lease means, and the concrete property of the aircraft of same model is still variant, and this illiteracy plate provides the means of interpolation adjustment easily for revising takeoff data fast.
4) the airport characteristic is covered plate, and the main service condition concrete according to airline provides the often quick correction illiteracy plate of the conditions such as high-altitude aerodrome, high temperature airport and airport, dash road of operation of airline.
5) flight planning is revised and is covered plate, and in-flight daily, flight planning often needs to revise, and for this reason, covers plate for the user provides a flight planning to revise.In daily use, the aircrew also can utilize this to cover plate and preset alternate flight plan.
Below by the design action pane picture example further specify the foregoing description.These action pane picture exhibitions are on the display panel of existing multi-functional control display unit.
Fig. 4 is the flight management system initialization page, inserts corresponding data in each input frame, finishes the initialization of desired data.
The description of contents of the next stage page that each choice box enters among Fig. 4 is as follows:
" Company Flight Plan " choice box should enter Company Flight Plan's page, and this page is all Company Flight Plans of alphabetically arranging, and is used for searching and selecting;
" air route selection " choice box should enter the air route and select the page, and this page is all air routes of alphabetically arranging, and the code that takes off/arrive at the airport, and is used for searching and selecting;
Click " inertial reference system " choice box, enter the inertial reference system page, this page comprises selection and the gyrocompass alignment of IRS;
The choice box of " leaving the theatre " enters the departure procedure page, this page for this reason the airport all with the tactic runway of digital alphabet, be used for searching and selecting.After selecting a runway, the page switch for this reason runway operable all with the tactic standard instrument departure, SID mission program of digital alphabet (SID) program, be used for searching and select (if not having corresponding SID then to select NONE (nothing)).After selecting SID, the page switch for this reason runway operable all with the tactic standard instrument departure, SID transient program of digital alphabet (SID TRANSITION) program, be used for searching and select (if not having corresponding SID TRANSITION then to select NONE).
" navigation " choice box, this page are that navigate mode is selected, as shown in Figure 5.Navigate mode is (according to a priority order):
GPS (GPS)
DME/DME (DME/DME) (viameter/viameter)
VOR/DME (VOR/DME) (nodirectional beacon/viameter)
IRS (inertial reference system)
Dead reckoning
Every kind of navigate mode also should provide its longitude and latitude that calculates and EPU (the aircraft position inaccuracy of estimation, just a kind of scope of permissible variation).
Load and fuel oil, this page are the input and the demonstration of load and fuel oil.As shown in Figure 6, comprising:
Empty-weight comprises the aircraft zero load, the weight of equipment and unit.
Load type, the weight on the machine of goods.
Ridership/average weight, the quantity of Passenger On Board, and their average weight.
Cost index.
The fuel oil gross weight, the weight of fuel oil on the machine.
Fuel Remained, Fuel Remained weight.
Refuel/drain the oil the weight of oiling (+) or drain the oil (-).
Fuel flow, unit K G/H.
Takeoff data, this page are the input of takeoff data and show as shown in Figure 7:
The air route guide look, this page is all air routes of alphabetically arranging, and the code that takes off/arrive at the airport, and is used for searching and selecting.As shown in Figure 8.
Click " data " in the master menu hurdle, select " pilot's data " page, as shown in Figure 9:
Pilot's page of data is as shown in figure 10:
Messaging list: the warning that display priority is the highest.Click enters, and can check all alert messages.
Attention: no matter on any page, this journey should show all the time.
The edit page of flight planning as shown in figure 11, show the time, speed of each way point in the flight planning, highly, Fuel Remained (EFOB) information on the flight path, distance, machine, the time can show estimated time of arrival (ETA) or leg estimation flight time (ETE).Click " flight planning historical record " button and can check the way point information of having flown over.Click " search and rescue aid " button and enter the search and rescue aid pattern.
The way point of flight planning and the modification of leg are entered by flight planning list inlet, as shown in figure 12.The pilot can revise flight planning at any time.The level revision that the pilot can carry out has: deletion/insertion way point, departure procedure (takeoff runway, conversion in SID and the way), arrival procedure (runway, advance nearly type, STAR, advance nearly conversion, conversion etc. in the way), leg, holding patterrn, alternate airport, the vertical revision that the pilot can carry out has: time restriction, speed limit, limitation in height, height of lift, wind, Mach constant leg.
Way point to appointment:
Choose " flying nonstop to * from current location ", the way point between current location (PPOS) and this way point all will deletion from the flight planning tabulation.
Choose " inserting next way point ", will after this way point, insert a way point.
Choose " deletion ", this way point will deletion from the flight planning tabulation.
Choose " departure procedure ", enter " leaving the theatre " page, can revise the information of leaving the theatre, have only that to be in when leaving the theatre the leg this option optional when this way point.
Choose " arrival procedure ", enter " marching into the arena " page, can revise the information of marching into the arena, have only that to be in when marching into the arena the leg this option optional when this way point.
Choose " departing from ", will show its submenu, clicking upper and lower arrow can increase and reduce left and right sides side-play amount.
Choose " holding patterrn ", this way point is added to etc. in the course line.
Choose " leaping ", this way point is configured to force to leap a little.
Choose " enabling alternate airport ", from this way point alternate airport that flies to.
Choose " new destination ", from this way point new destination of flying to.
Choose " restriction ", show its submenu, can revise limitation in height, speed limit, time restriction (RTA) etc.
Mach constant leg: Mach constant value.
Choose " height of lift ", be set in the height of lift of this way point, click upper and lower arrow and can increase, subtract the height of lift value.
Wind, current wind speed.
Claims (8)
1, a kind of input media of electronic system of civil aircraft control cabin is characterized in that comprising:
Aircraft performance database and navigational route database are stored with aeroplane performance data and navigation data;
Property database, be connected with navigational route database with described aircraft performance database, be stored with the takeoff data that generates according to the data of storing in described aircraft performance database and the navigational route database, the data of climbing, the data of cruising, following drop data, advance nearly data, landing data;
Cover the plate database, be connected, be used for obtaining data, be stored with the fundamental characteristics of setting according to aeroplane performance and cover plate from described property database with described property database; The mission phase of setting according to aerial mission covers plate; Flying experience according to course line and technical characterictic setting is covered plate;
The multi-functional control display unit is connected with described illiteracy plate database, is used for according to covering the interface that the plate database provides data input and control being carried out in control of aircraft cockpit associated electrical and management system.
2, a kind of input method of electronic system of civil aircraft control cabin is characterized in that: comprise and cover the plate database, be stored with the fundamental characteristics of setting according to aeroplane performance and cover plate; The mission phase of setting according to aerial mission covers plate; Flying experience according to course line and technical characterictic setting is covered plate; By covering the illiteracy board interface that the plate database provides, data input and control are carried out in control of aircraft cockpit associated electrical and management system.
3, the input method of electronic system of civil aircraft control cabin according to claim 2 is characterized in that: the data that described fundamental characteristics covers the plate processing comprise:
1) aeroplane performance basic parameter input;
2) initialization data of On-board Navigation resource.
4, according to the input method of claim 2 or 3 described electronic system of civil aircraft control cabin, it is characterized in that: described mission phase covers plate for covering plate in conjunction with the type characteristic according to the instrument flight procedure of seaworthiness requirements set, comprise prepare, slide, take off, climb, cruise, descend, advance closely before the flight, landing period.
5, the input method of electronic system of civil aircraft control cabin according to claim 4, it is characterized in that: described mission phase covers plate and also comprises modification stage, described modification stage: modification stage comprises that horizontal cross-section is revised data and vertical section is revised data options.
6, the input method of electronic system of civil aircraft control cabin according to claim 5 is characterized in that: the preparatory stage deal with data comprises before the described flight:
Take off and weather environment data, load data, fuel oil data, the weight balancing data of landing station;
The navigation resource data that this flight is required;
The instrument program data that this flight is performed;
The ground navigation aid platform data that this flight is performed;
The emergency procedure data that this flight is performed;
The flight plan data that this flight is performed;
The data that handle described coast period comprise:
Preset the coasting time and the fuel oil data of corresponding airfield runway;
By recomputating of time and fuel oil data, real-time update flight planning;
The equilibrium point of calculation fuel consume;
The data that handle described takeoff phase comprise:
The mode of taking off data;
The takeoff data data;
The operation inspection forms data;
The system operation program prompts;
The data that described ramp-up period is handled comprise:
The mode of climbing data;
The climbing performance data;
The system operation program prompts;
The data that described cruising phase is handled comprise:
The mode of cruising data;
The wind correction data of cruising;
The system operation program prompts;
The data that the described decline stage handles comprise:
Decline mode data;
The descent performance data;
The system operation program prompts;
The described data of advancing nearly phase process comprise:
Advance nearly mode data;
Advance nearly restricting data;
The system operation program prompts;
The data that described landing period is handled comprise:
Landing data;
Speed limit data;
The system operation program prompts.
7, according to the input method of claim 5 or 6 described electronic system of civil aircraft control cabin, it is characterized in that: it is for airline provides a cover self-defining illiteracy plate that described flying experience is covered plate, comprises course line characteristic, airmanship experience, fuel oil and economic policies and the feature scheme formulated.
8, the input method of electronic system of civil aircraft control cabin according to claim 7 is characterized in that: described flying experience cover plate comprise in the following illiteracy plate partly or entirely:
1) the meteorological condition experience is covered plate: at the feature of local meteorological condition, set company's predetermined process principle;
2) the ground queuing is taken off and is waited for illiteracy plate, the amendment scheme of setting at hub;
3) the type take-off and landing characteristic is covered plate, the amendment scheme data of setting according to the concrete feature of aircraft configuration;
4) the airport characteristic is covered plate, and the service condition concrete according to airline provides the often quick correction illiteracy plate of high-altitude aerodrome, high temperature airport and airport, the dash road condition of operation of airline;
5) flight planning is revised and is covered plate, revises the illiteracy plate for the flight planning that the user provides, and the aircrew also can utilize this illiteracy plate to preset alternate flight plan.
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| CNA2008102021026A CN101403898A (en) | 2008-10-31 | 2008-10-31 | Input method and apparatus for electronic system of civil aircraft control cabin |
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| CN107195202A (en) * | 2016-03-15 | 2017-09-22 | 空中客车运营简化股份公司 | Center is assisted in flight management for multiple aircraft |
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| CN110889980A (en) * | 2018-09-11 | 2020-03-17 | 波音公司 | Method and device for providing an aircraft with a continuous flight trajectory |
| CN110889980B (en) * | 2018-09-11 | 2023-04-11 | 波音公司 | Method and computing device for controlling an aircraft |
| CN112445459A (en) * | 2019-08-28 | 2021-03-05 | 安徽华明航空电子系统有限公司 | Design method of flight management system |
| CN111063220A (en) * | 2019-11-28 | 2020-04-24 | 中国航空工业集团公司西安航空计算技术研究所 | General aircraft flight plan management system |
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