CN103295447A - Real-time flight parameter acquiring and transmitting system for full flight simulator - Google Patents
Real-time flight parameter acquiring and transmitting system for full flight simulator Download PDFInfo
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- CN103295447A CN103295447A CN2013101838558A CN201310183855A CN103295447A CN 103295447 A CN103295447 A CN 103295447A CN 2013101838558 A CN2013101838558 A CN 2013101838558A CN 201310183855 A CN201310183855 A CN 201310183855A CN 103295447 A CN103295447 A CN 103295447A
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Abstract
The invention provides a real-time flight parameter acquiring and transmitting system for a full flight simulator. The real-time flight parameter acquiring and transmitting system comprises a flight parameter acquiring module and a flight parameter transmitting module which are mutually connected. The flight parameter acquiring module is embedded to a simulator mainframe of a simulator system for simulating flight environment and acquires flight parameter data in real time during flight simulation of the simulator. The flight parameter transmitting module transmits the acquired flight parameter data to process by a land and air calling terminal of the simulator system through the network. Requirements of an analog simulation system for real-time data acquiring can be met, so that the simulator can function in flight training of regular or non-regular subjects instead of real civil aircrafts, and training quality is effectively improved and training cost is reduced.
Description
Technical field
The present invention relates to the system of a kind of real-time collection full dynamic simulated machine flight parameter and real-time Transmission, belong to aviation flight person and train the field.
Background technology
Full dynamic simulated machine occupies important status in civil aviation training field, it implements purpose is analogue simulation civil aircraft all sense organ performances under the normal condition and under the improper situation in the Live Flying environment as much as possible, play and replace true civil aircraft to carry out normal subject and the purpose flight training effect of improper section, effectively enhancement training quality and reduction training cost.
In the Live Flying environment, the pilot need defer to all kinds of air control instructions and make suitably and replying.This process comprises the wireless station that the frequency modulation that is in due course is suitable, and report current flight situation data are also intercepted the instruction that relevant air control person sends, and the instruction of execution air control is also made and being replied.The control dialogue that we are referred to as control unit and interplane in this spacelike is the empty conversation in land, and the empty conversation in land is the significant process that runs through whole flight course and be related to flight safety.Need analogue simulation is carried out in this type of conversation in the flight environment of vehicle simulation, and the content of the empty conversation in this type of land is the real-time reflection to flight environment of vehicle, so analog machine needs to gather in real time the various flying qualities in the simulated flight environment.
Summary of the invention
In order to satisfy needs often, the present invention proposes the system of a kind of real-time collection full dynamic simulated machine flight parameter and real-time Transmission, realize real-time flight, state parameter collection, the sending function of analog machine training.Every analog machine disposes corresponding flying quality collection and sending module, can independently finish parameter acquisition, the sending function of this analog machine.
Technical scheme of the present invention comprises:
The system of a kind of real-time collection full dynamic simulated machine flight parameter and real-time Transmission, comprise interconnected flight parameter acquisition module and transport module, described flight parameter module is embedded into the analog machine main frame for the simulator system of flight environment of vehicle simulation, in the process of analog machine simulated flight, gather the flight parameter data in real time, the empty call terminal in land that the flight parameter data of gathering send to simulator system is handled by network by described transport module.
As a kind of improvement of above technical scheme, the flight parameter of flight parameter acquisition module collection comprises airport code, runway code, radio altitude, aircraft transit square degree and air speed.
As a kind of improvement of above technical scheme, the data transmission format of described transport module is floating number and Boolean, and the flight parameter with collection on the 10HZ frequency sends the empty call terminal in land to.
As a kind of improvement of above technical scheme, described transport module is connected by the empty call terminal in TCP/IP network and land.
The system of the present invention required analog machine flight of real-time acquisition system on request, state parameter, carry out standard, form mathematical operation conversion in case of necessity, generate the flight parameter data message, and will gather the flight parameter data message that generates and press setup time at interval, be sent to the empty verbal system/common apparatus in corresponding simulating machine land and system's supervisory control desk module by the TCP/IP procotol.
System configuration of the present invention is on analog machine, in all kinds of flight subject training, realize gathering in real time flight parameter, according to relevant land empty conversation principle and mechanism, intelligence generates the audio frequency output of various calls, the empty call voice environment in the land of simulation Live Flying and scene, and then satisfy the needs of high analogue simulation machine system, analog machine is played replace true civil aircraft to carry out normal subject and the purpose flight training effect of improper section, effectively enhancement training quality and reduce the training cost.
Description of drawings
Below with reference to accompanying drawing and example the present invention is further specified, wherein:
Fig. 1 is equipment synoptic diagram of the present invention;
Fig. 2 is flight parameter collecting flowchart figure of the present invention.
Embodiment
The collection full dynamic simulated machine flight parameter that the present invention proposes and the system of real-time Transmission are applicable to analog machine land empty conversation environmental simulation system and are used, and are configured in the full dynamic simulated machine, constitute the simulator system of a complete simulated flight environment.This parameter acquisition realizes gathering in real time flight parameter with being transmitted in the training of all kinds of flight subjects, by the empty verbal system terminal basis relevant land empty conversation principle in land and mechanism, intelligence generates the audio frequency output of various calls, the empty call voice environment in the land of simulation Live Flying and scene.
Referring to Fig. 1, this type of simulator system comprises full dynamic simulated machine usually, and this full dynamic simulated machine contains the analog machine main frame of controlling usefulness, and the analog machine main frame is connected with the empty call terminal in land.Wherein, the flight parameter acquisition module that native system comprises is embedded into and carries out data acquisition in the analog machine main frame, and the information of collection sends to the empty call terminal in land by output module and handles.System also comprises the empty verbal system main frame in land that is connected by the empty call terminal in TCP/IP network and land, main frame is provided with the control zone multi-dimensional database, this database is the multidimensional data model maintenance database of all kinds of blank pipe area controls, be the data source of the identification of blank pipe zone, decision algorithm, comprise all kinds of blank pipes zone and mass data.
Shown in the process flow diagram among Fig. 2, system of the present invention at first carries out data, buffer zone and communication protocol initialization, activation is embedded into the flight parameter acquisition module in the full dynamic simulated machine, obtain analog machine BSD data, again the data of gathering are carried out standard, format conversion, generate the communication data message, by the TCP/IP network supplemental characteristic is sent to the empty call terminal in land through transport module, the database that finally calls end host carries out data to be handled.In addition, system of the present invention also has unusually, mistake is handled and report to the police, repair mechanism automatically, can in time advance robotization when unusual, mistake in parameter acquisition, occurring and handle.
Wherein, the flight parameter of collection comprises airport code, runway code, radio altitude, aircraft transit square degree and air speed.The data transmission format of transport module is floating number and Boolean, and the flight parameter with collection on the 10HZ frequency sends the empty call terminal in land to.Transport module is connected by the empty call terminal in TCP/IP network and land.
The system of the present invention required analog machine flight of real-time acquisition system on request, state parameter, carry out standard, form mathematical operation conversion in case of necessity, generate the flight parameter data message, and will gather the flight parameter data message that generates and press setup time at interval, be sent to the empty verbal system/common apparatus in corresponding simulating machine land and system's supervisory control desk module by the TCP/IP procotol.
System configuration of the present invention is on analog machine, in all kinds of flight subject training, realize gathering in real time flight parameter, according to relevant land empty conversation principle and mechanism, intelligence generates the audio frequency output of various calls, the empty call voice environment in the land of simulation Live Flying and scene, and then satisfy the needs of high analogue simulation machine system, analog machine is played replace true civil aircraft to carry out normal subject and the purpose flight training effect of improper section, effectively enhancement training quality and reduce the training cost.
The above is preferred embodiment of the present invention, and the present invention is not limited to above-mentioned embodiment, as long as it reaches technique effect of the present invention with identical means, all should belong to protection scope of the present invention.
Claims (4)
1. system of gathering in real time full dynamic simulated machine flight parameter and real-time Transmission, it is characterized in that, comprise interconnected flight parameter acquisition module and transport module, described flight parameter module is embedded into the analog machine main frame for the simulator system of flight environment of vehicle simulation, in the process of analog machine simulated flight, gather the flight parameter data in real time, the empty call terminal in land that the flight parameter data of gathering send to simulator system is handled by network by described transport module.
2. the system of real-time collection full dynamic simulated machine flight parameter according to claim 1 and real-time Transmission, it is characterized in that the flight parameter of described flight parameter acquisition module collection comprises airport code, runway code, radio altitude, aircraft transit square degree and air speed.
3. the system of real-time collection full dynamic simulated machine flight parameter according to claim 1 and real-time Transmission, it is characterized in that, the data layout of described transport module transmission is floating number and Boolean, and the flight parameter with collection on the 10HZ frequency sends the empty call terminal in land to.
4. the system of real-time collection full dynamic simulated machine flight parameter according to claim 1 and real-time Transmission is characterized in that, described transport module is connected by the empty call terminal in TCP/IP network and land.
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Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104133378B (en) * | 2014-08-05 | 2017-01-25 | 中国民用航空总局第二研究所 | Real-time simulation platform for airport activity area monitoring guidance system |
CN108665761A (en) * | 2018-05-18 | 2018-10-16 | 中国民航大学 | A kind of flight data recording system Practical Teaching Platform |
CN110223565A (en) * | 2019-06-25 | 2019-09-10 | 深圳市道通智能航空技术有限公司 | A kind of flight simulation method, device, equipment and storage medium |
CN114638442A (en) * | 2022-05-19 | 2022-06-17 | 珠海翔翼航空技术有限公司 | Flight training scheme generation system, method and equipment for individual difference |
CN115909820A (en) * | 2022-11-04 | 2023-04-04 | 上海华模科技有限公司 | Training method and system for coping with air traffic control and corresponding storage medium |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1521655A (en) * | 2003-01-28 | 2004-08-18 | 中国南方航空股份有限公司 | Computer-aided teaching system and method for stimulated aviation training |
RU2250511C1 (en) * | 2004-03-10 | 2005-04-20 | ОАО "ОКБ им. А.С. Яковлева" | Aircraft training complex |
CN101739860A (en) * | 2009-11-30 | 2010-06-16 | 四川川大智胜软件股份有限公司 | System for making radar simulator training plan based on real radar data |
CN101739859A (en) * | 2009-11-30 | 2010-06-16 | 四川川大智胜软件股份有限公司 | Scene surveillance radar simulation system |
CN102053563A (en) * | 2010-12-27 | 2011-05-11 | 刘宇 | Flight training data acquisition and quality evaluation system of analog machine |
-
2013
- 2013-05-17 CN CN201310183855.8A patent/CN103295447B/en active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1521655A (en) * | 2003-01-28 | 2004-08-18 | 中国南方航空股份有限公司 | Computer-aided teaching system and method for stimulated aviation training |
RU2250511C1 (en) * | 2004-03-10 | 2005-04-20 | ОАО "ОКБ им. А.С. Яковлева" | Aircraft training complex |
CN101739860A (en) * | 2009-11-30 | 2010-06-16 | 四川川大智胜软件股份有限公司 | System for making radar simulator training plan based on real radar data |
CN101739859A (en) * | 2009-11-30 | 2010-06-16 | 四川川大智胜软件股份有限公司 | Scene surveillance radar simulation system |
CN102053563A (en) * | 2010-12-27 | 2011-05-11 | 刘宇 | Flight training data acquisition and quality evaluation system of analog machine |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104133378B (en) * | 2014-08-05 | 2017-01-25 | 中国民用航空总局第二研究所 | Real-time simulation platform for airport activity area monitoring guidance system |
CN108665761A (en) * | 2018-05-18 | 2018-10-16 | 中国民航大学 | A kind of flight data recording system Practical Teaching Platform |
CN110223565A (en) * | 2019-06-25 | 2019-09-10 | 深圳市道通智能航空技术有限公司 | A kind of flight simulation method, device, equipment and storage medium |
CN110223565B (en) * | 2019-06-25 | 2022-02-22 | 深圳市道通智能航空技术股份有限公司 | Flight simulation method, device, equipment and storage medium |
CN114638442A (en) * | 2022-05-19 | 2022-06-17 | 珠海翔翼航空技术有限公司 | Flight training scheme generation system, method and equipment for individual difference |
CN115909820A (en) * | 2022-11-04 | 2023-04-04 | 上海华模科技有限公司 | Training method and system for coping with air traffic control and corresponding storage medium |
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