CN101587506A - Flight procedure aided design device - Google Patents
Flight procedure aided design device Download PDFInfo
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- CN101587506A CN101587506A CNA2009100858276A CN200910085827A CN101587506A CN 101587506 A CN101587506 A CN 101587506A CN A2009100858276 A CNA2009100858276 A CN A2009100858276A CN 200910085827 A CN200910085827 A CN 200910085827A CN 101587506 A CN101587506 A CN 101587506A
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Abstract
A kind of flight procedure aided design device is disclosed; comprise mission program basic data establishment/editor module, traditional mission program template instrument establishment/editor module, traditional mission program standard protected location drafting, evaluation module, graphic plotting module, auxiliary computing module, chart making module, its design mission program reports the procedure chart and the protected location figure of use.This device is on the basis that meets International Civil Aviation Organization's relevant criterion, by to the spatial domain with the mission program design function of robotization is provided, for the mission program design effort provides design means and support.
Description
Technical field
The present invention relates to a kind of termination environment mission program design apparatus, the design and the apparatus for evaluating of the mission program under especially traditional navigate mode.
Background technology
Mission program work is an important process that guarantees flight and blank pipe commander safety, also is the basic foundation of airport addressing, guidance station layout and termination environment airspace management.The mission program design needs lot of data calculating, protected location to draw and map homework, and handwork is complicated, and workload is big, and precision is difficult to guarantee.Along with computer technology and DEVELOPMENT OF GEOGRAPHICAL INFORMATION SYSTEM, computer-aided design (CAD) has become the important means of mission program design.
At present, domestic standard of carrying out the mission program design is: " the visual and instrument flight procedure design of the file DOC8168-POS/611 of International Civil Aviation Organization " aerial navigation service routine---aircraft operation " second volume.In concrete work, the each department programmer exists difference for the understanding of 8168 corresponding clauses, and the disunity in this understanding has caused the disunity of various places in the standard of carrying out mission program design time institute's foundation.Do not have standard, do not have standard, just produced authority.This authority will form huge obstacle from long term growth for CAAC's mission program design effort.
In order to reverse present this situation, the actual understanding and the demand of comprehensive each department management board, build unified " flight procedure aided design device " in a cover whole nation, job guide and aid as the program design staff will have important and practical meanings.Simultaneously, set up unified " flight procedure aided design device ", also with the standardization and the standardization construction of strong promotion mission program design, for construction " the CAAC's mission program design specifications " with distinct distinct Chinese characteristics that tally with the national condition lays the foundation.
Along with the fast development of China's economic, every business of CAAC is also in the speed increment that surpasses 20% with every year.During the 11th Five-Year, the quantity of the annual newly-built airports of China increases sharply, and simultaneously, it is civilian to also have a large amount of military airfields to transfer to.In order to make these airport securities, to come into operation efficiently, need the mission program designer of various places to do a large amount of work.
What form distinct contrast therewith is that present national civil aviaton is engaged in the about altogether 30-40 people of personnel of mission program design.And the mission program designer who cultivates a maturation needs the time of 2-3 at least, and therefore, in the quite a long time, personnel's deficiency will be a conspicuous contradiction of restriction mission program designs afterwards.The most real solution for this kind situation is exactly to excavate the potentiality of current procedure design effort, increases work efficiency.And the most direct effective way of increasing work efficiency is improved instrument exactly---set up the perfect mission program design apparatus of a cover.
Summary of the invention
The technical problem to be solved in the present invention has provided a kind of flight procedure aided design device of high efficiency.
Technical scheme of the present invention is: this flight procedure aided design device comprises: mission program basic data establishment/editor module, and it creates general spatial domain fundamental element and particular design object that mission program uses; Tradition mission program template instrument establishment/editor module, it uses the specific template instrument that defines in the ICAO DOC-8168 standard, and design drawing template commonly used; Draw tradition mission program standard protected location, evaluation module, and it draws accurate, each stage protected location of the traditional mission program of non-precision, and the barrier in the protected location is surpassed barrier evaluation; The graphic plotting module, it carries out assisting in flying programmed protection district graphic designs, and finishes special pattern and draw; Auxiliary computing module, it is used the mission program complicated formulas always and calculates, and design aids such as signal covering, minimum operation standard are provided; Chart is made module, and its design mission program reports the procedure chart and the protected location figure of use.
This device is on the basis that meets International Civil Aviation Organization's relevant criterion, by to the spatial domain with the mission program design function of robotization is provided, for the mission program design effort provides design means and support.It has solved that mission program design data calculation of complex, protected location draw that handwork is complicated, workload big, precision is difficult to guarantee and since designer's level differ bring standard is understood skimble-scamble problem.
Description of drawings
Fig. 1 is a functional block diagram of the present invention;
Fig. 2 is the functional block diagram of mission program basic data establishment/editor module;
Fig. 3 is the functional block diagram of traditional mission program template instrument establishment/editor module;
Fig. 4 is that draw traditional mission program standard protected location, the functional block diagram of evaluation module;
Fig. 5 is the functional block diagram of graphic plotting module;
Fig. 6 is the functional block diagram of auxiliary computing module;
Fig. 7 makes the functional block diagram of module for chart;
Fig. 8 is the process flow diagram of the method for the standard protected location drawing unit in the drafting of traditional mission program standard protected location, the evaluation module;
Fig. 9 is the process flow diagram of the method for the standard protected location assessment unit in the drafting of traditional mission program standard protected location, the evaluation module.
Embodiment
Below by drawings and Examples, technical scheme of the present invention is described in further detail.
Fig. 1 is a functional block diagram of the present invention.This flight procedure aided design device comprises: mission program basic data establishment/editor module, and it creates general spatial domain fundamental element and particular design object that mission program uses; Tradition mission program template instrument establishment/editor module, the specific template instrument that defines in its processing IC AODOC-8168 standard, and design drawing template commonly used; Draw tradition mission program standard protected location, evaluation module, and it draws accurate, each stage protected location of the traditional mission program of non-precision, and the barrier in the protected location is surpassed barrier evaluation; The graphic plotting module, it carries out assisting in flying programmed protection district graphic designs, and finishes special pattern and draw; Auxiliary computing module, it is used the mission program complicated formulas always and calculates, and design aids such as signal covering, minimum operation standard are provided; Chart is made module, and its design mission program reports the procedure chart and the protected location figure of use.
Fig. 2 is the functional block diagram of mission program basic data establishment/editor module.Preferably, described mission program basic data establishment/editor module comprises: basic spatial domain element creating unit, create spatial domain element commonly used in the environment of civil aviation spatial domain, as spatial domain objects such as guidance station, runway, air routes; Mission program design element creating unit is created the spatial domain object at mission program design specific needs, as barrier, cross bearing point, mistake platform anchor point, specific turning flight path etc.
Fig. 3 is the functional block diagram of traditional mission program template instrument establishment/editor module.Preferably, described traditional mission program template instrument establishment/editor module comprises: 8168 definition protected location modular units, draw in 8168 in order to simplify the standard protected location template of drawing protection drawing process definition, as right angle template, wait template, OAS template etc.; The drawing template unit that design is commonly used is drawn drawing element commonly used in the mission program design effort, as was led platform anchor point tolerance template, cross bearing point tolerance template, guide table template and side platform template etc.
Fig. 4 is that draw traditional mission program standard protected location, the functional block diagram of evaluation module.Preferably, described traditional mission program standard protected location drafting, evaluation module comprise:
(1) standard protected location drawing unit, main being responsible for finished the required corresponding protected location of user according to guidance station, runway information.Wherein, the standard protected location is the protected location pattern of clearly stipulating in the DOC-8168 file.This device provides the drafting and the modify feature of several protected locations commonly used, comprises that straight-line approach protected location, straight line are left the theatre (the platform guiding is arranged), straight line is left the theatre (no platform guiding), the DME arc is marched into the arena the protected location, DME arc Initial Approach protected location, minimum sector altitude, visually spirals, the base turn protected location, waits for protected location, box pattern protected location, OAS face, accurate middle drafting of entering common protected locations such as nearly protected location, U type protected location, S type protected location.When drawing; draw the protected location of each leg according to the correlation parameter of regulation in 8186; fundamental purpose provides to a half-finished protected location of user object; the user can revise attribute information by corresponding property box then; also can be by in map window, changing the outward appearance of protected location; change corresponding attribute, till reaching designing requirement.Wherein, Fig. 8 is the process flow diagram of the method for standard protected location drawing unit.This method mainly may further comprise the steps: (1) need to select the protected location type of design, and it is dragged and dropped in the design effort district; (2) the protected location attribute is set, thereby changes protected location profile or gradient, reach the purpose of keeping away barrier; (3) the barrier evaluation is carried out in the protected location, the control barrier in the district that is protected; (4) judge the super barrier degree in protected location; (5) repeating step (2)-(4) are adjusted protected location profile and parameter repeatedly, enable to meet design requirement.
(2) standard protected location assessment unit, main being responsible for carried out multi-form Function of Evaluation to the protected location, and with the data source of evaluation result as chart output.The protected location is estimated according to the stage in air route and differently with type mainly is divided into two kinds of evaluation methods: high evaluation and gradient evaluation.The former mainly assesses the requirement for height whether protected location meets design, and whether the air route section that the latter mainly assesses design satisfies the gradient requirement that designs.Wherein, Fig. 9 is the process flow diagram of the method for standard protected location assessment unit.This method mainly may further comprise the steps: (1) selects the protected location of needs assessment; (2) the evaluation type of selection protected location can be estimated digital elevation model (Digital Elevation Model, vehicle economy M) barrier, also can estimate the cultural obstacle of the manual input of designer; What (3) the judgement designer selected is to estimate DEM barrier or evaluation cultural obstacle; (4) if estimate cultural obstacle, then extract the cultural obstacle that comprises in the spatial dimension of place, protected location; (5), then need to intercept the dem data in the scope of protected location if estimate the DEM barrier; (6) calculate the spatial relationship between each spot elevation and protected location in the dem data intercepted; (7) calculate the super barrier situation of each barrier; (8) relatively draw the control barrier of protected location; (9) result of calculation is shown to the designer with the form of tabulating and carries out reference.
(3) standard protected location property control unit, the main demonstration of being responsible for control protected location attribute is the interactive interface that the user edits the protected location and carries out the barrier assessment.
Fig. 5 is the functional block diagram of graphic plotting module.Preferably, described graphic plotting module comprises:
(1) graphic plotting unit; mainly finish the drafting and the relevant information modify feature of pure figure; used most figure in accurately charting is provided; be primarily aimed at the processing of the linking section between the protected location and in whole mission program design process, provide some non-productive operations, comprise the drafting of following several figures: point, text, mark along the line, straight line, parallel lines, multistage line, tangent line, circular arc, curve, free curve, conch line, rectangle, polygon, parallelogram, circle.
(2) graphics edition unit; can finish accurately the moving of figure or protected location object, bi-directional scaling very easily, rotate operation such as a certain angle accurately; mainly be to provide fast and accurately auxiliary solution to accurate drawing, this device mainly provides following several function: accurately move, mirror image, skew, accurate rotation, convergent-divergent, connection, prolongation, pruning, extend, interrupt, fillet, align, be converted into face, be converted into line, line, merging, common factor, difference set, symmetric difference set, buffer zone.
Fig. 6 is the functional block diagram of auxiliary computing module.Preferably, described auxiliary computing module comprises: the computational tool unit, be device provide some about designed some pure mathematics computing instruments that arrive in the mission program design process, do the computing work of some manual verifications to make things convenient for the user; Airport minimum operation standard block is to formulate the aircraft instrument that the minimum operation standard provides on corresponding runway for the user on the basis of advancing near and overshoot flight phase evaluation result.
Fig. 7 makes the functional block diagram of module for chart.Preferably, described chart is made module and is comprised: the procedure chart production unit, employed guidance station planimetric map, guidance station sectional view, runway enroute chart and some other legends in the instrument of publishing picture are provided, and basic material is provided for publishing picture; Protected location figure production unit; according to civil aviaton's standard of publishing picture content in the current map viewing area is switched in the map viewing area at " topological design " interface; in to have established general placement scheme available, can modify and illustrate the protected location that designs, and engineer's scale is set publishes picture.
The above; it only is preferred embodiment of the present invention; be not that the present invention is done any pro forma restriction, every foundation technical spirit of the present invention all still belongs to the protection domain of technical solution of the present invention to any simple modification, equivalent variations and modification that above embodiment did.
Claims (7)
1, flight procedure aided design device is characterized in that, this device comprises:
Mission program basic data establishment/editor module, it creates general spatial domain fundamental element and particular design object that mission program uses;
Tradition mission program template instrument establishment/editor module, it uses the specific template instrument that defines in the ICAO DOC-8168 standard, and design drawing template commonly used;
Draw tradition mission program standard protected location, evaluation module, and it draws accurate, each stage protected location of the traditional mission program of non-precision, and the barrier in the protected location is surpassed barrier evaluation;
The graphic plotting module, it carries out assisting in flying programmed protection district graphic designs, and finishes special pattern and draw;
Auxiliary computing module, it is used the mission program complicated formulas always and calculates, and design aids such as signal covering, minimum operation standard are provided;
Chart is made module, and its design mission program reports the procedure chart and the protected location figure of use.
2, flight procedure aided design device according to claim 1 is characterized in that, described mission program basic data establishment/editor module comprises:
Basic spatial domain element creating unit, it creates spatial domain element commonly used in the environment of civil aviation spatial domain;
Mission program design element creating unit, it creates the spatial domain object at mission program design specific needs.
3, flight procedure aided design device according to claim 1 is characterized in that, described traditional mission program template instrument establishment/editor module comprises:
8168 definition protected location modular units, it is drawn in 8168 in order to simplify the standard protected location template of drawing protection drawing process definition;
The drawing template unit that design is commonly used, it draws drawing element commonly used in the mission program design effort.
4, flight procedure aided design device according to claim 1 is characterized in that, draw described traditional mission program standard protected location, evaluation module comprises:
Standard protected location drawing unit, it finishes the design of the required corresponding protected location of user according to guidance station, runway information;
Standard protected location assessment unit, it carries out multi-form evaluation to the protected location, and with the data source of evaluation result as chart output;
Property control unit, standard protected location, the demonstration of its control protected location attribute.
5, flight procedure aided design device according to claim 1 is characterized in that, described graphic plotting module comprises:
The graphic plotting unit, it carries out the drafting of pure figure and the modification of relevant information;
The graphics edition unit, it is operated figure or protected location object, and provides auxiliary to accurate drawing.
6, flight procedure aided design device according to claim 1 is characterized in that, described auxiliary calculating mould module comprises:
The computational tool unit, it provides about pure mathematics computing instrument involved in the mission program design process;
Airport minimum operation standard block, it provides the minimum operation standard of aircraft on corresponding runway.
7, flight procedure aided design device according to claim 1 is characterized in that, described chart is made module and comprised:
The procedure chart production unit, it provides employed legend in the instrument of publishing picture;
Protected location figure production unit, it switches to content in the current map viewing area in the map viewing area at " topological design " interface according to civil aviaton's standard of publishing picture, and is provided with general placement scheme.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA2009100858276A CN101587506A (en) | 2009-06-01 | 2009-06-01 | Flight procedure aided design device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA2009100858276A CN101587506A (en) | 2009-06-01 | 2009-06-01 | Flight procedure aided design device |
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| CN101587506A true CN101587506A (en) | 2009-11-25 |
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| CNA2009100858276A Pending CN101587506A (en) | 2009-06-01 | 2009-06-01 | Flight procedure aided design device |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103400018A (en) * | 2013-07-12 | 2013-11-20 | 中国民用航空飞行校验中心 | Flight program check and verification system and method |
| CN109615134A (en) * | 2018-12-10 | 2019-04-12 | 中国民用航空飞行学院 | One kind is left the theatre course data processing system and method, information data processing terminal |
-
2009
- 2009-06-01 CN CNA2009100858276A patent/CN101587506A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103400018A (en) * | 2013-07-12 | 2013-11-20 | 中国民用航空飞行校验中心 | Flight program check and verification system and method |
| CN103400018B (en) * | 2013-07-12 | 2016-03-09 | 中国民用航空飞行校验中心 | The system and method for a kind of flight program check and checking |
| CN109615134A (en) * | 2018-12-10 | 2019-04-12 | 中国民用航空飞行学院 | One kind is left the theatre course data processing system and method, information data processing terminal |
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Open date: 20091125 |