CN103295447B - A kind of Real-time Collection full dynamic simulated machine flight parameter the system of real-time Transmission - Google Patents
A kind of Real-time Collection full dynamic simulated machine flight parameter the system of real-time Transmission Download PDFInfo
- Publication number
- CN103295447B CN103295447B CN201310183855.8A CN201310183855A CN103295447B CN 103295447 B CN103295447 B CN 103295447B CN 201310183855 A CN201310183855 A CN 201310183855A CN 103295447 B CN103295447 B CN 103295447B
- Authority
- CN
- China
- Prior art keywords
- real
- flight parameter
- flight
- time
- collection
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Abstract
The present invention proposes a kind of Real-time Collection full dynamic simulated machine flight parameter and the system of real-time Transmission, it comprises the flight parameter acquisition module and transport module that are connected to each other, described flight parameter Module-embedding is in the analog machine main frame of the simulator system of simulating for flight environment of vehicle, Real-time Collection flight parameter data in the process of analog machine simulated flight, the empty call terminal in the land flight parameter data of collection being sent to simulator system by network by described transport module processes.The present invention can meet analogue simulation machine system to the needs of real time data acquisition, analog machine is played and replaces true civil aircraft to carry out normal subject and improper section object flight training effect, effective enhancement training quality and reduction training cost.
Description
Technical field
The present invention relates to a kind of Real-time Collection full dynamic simulated machine flight parameter and the system of real-time Transmission, belong to airline pilots and train field.
Background technology
Full dynamic simulated machine occupies very important status in civil aviation training field, it implements object is that analogue simulation civil aircraft shows with all sense organs under abnormal condition under normal circumstances in Live Flying environment as much as possible, play and replace true civil aircraft to carry out normal subject and improper section object flight training effect, effective enhancement training quality and reduction training cost.
In Live Flying environment, pilot needs defer to all kinds of air control instruction and make suitable response.This process comprises the suitable wireless station of the frequency modulation that is in due course, and reports current flight situation data and the instruction intercepted about air control person sends, and performs air control instruction and also makes response.The control that we are referred to as this kind of air control unit and interplane is talked with for land sky is conversed, and land sky call is the significant process running through whole flight course and be related to flight safety.Need to carry out analogue simulation to this type of call in flight environment of vehicle simulation, and the content of this type of land sky call is the real-time reflection to flight environment of vehicle, therefore analog machine needs the various flying qualities in Real-time Collection simulated flight environment.
Summary of the invention
In order to meet needs often, the present invention proposes a kind of Real-time Collection full dynamic simulated machine flight parameter and the system of real-time Transmission, realizing the real-time flight of analog machine training, state parameter collection, sending function.Every platform analog machine configures corresponding flying quality collection and sending module, can parameter acquisition, the sending function of this analog machine of complete independently.
Technical scheme of the present invention comprises:
A kind of Real-time Collection full dynamic simulated machine flight parameter the system of real-time Transmission, comprise the flight parameter acquisition module and transport module that are connected to each other, described flight parameter Module-embedding is in the analog machine main frame of the simulator system of simulating for flight environment of vehicle, Real-time Collection flight parameter data in the process of analog machine simulated flight, the empty call terminal in the land flight parameter data of collection being sent to simulator system by network by described transport module processes.
One as above technical scheme is improved, and the flight parameter of flight parameter acquisition module collection comprises airport code, runway code, radio altitude, aircraft transit square degree and air speed.
One as above technical scheme is improved, and the data transmission format of described transport module is floating number and Boolean, and the flight parameter of collection sends to the empty call terminal in land by 10HZ frequency.
One as above technical scheme is improved, and described transport module is connected by the empty call terminal in TCP/IP network and land.
System of the present invention can on request needed for real-time acquisition system analog machine flight, state parameter, carry out standard, form mathematical operation conversion if desired, generate flight parameter data message, and press interval setup time by gathering the flight parameter data message generated, be sent to the empty verbal system/common apparatus in corresponding analog machine land and system main-control platform module by TCP/IP procotol.
System configuration of the present invention is on analog machine, Real-time Collection flight parameter is realized in all kinds of flight subject training, according to relevant land sky call principle and mechanism, the audio frequency that intelligence generates various calls exports, the empty call voice environment in land of Reality simulation flight and scene, and then meet the needs of high analogue simulation machine system, analog machine is played and replaces true civil aircraft to carry out normal subject and improper section object flight training effect, effective enhancement training quality and reduction training cost.
Accompanying drawing explanation
Below with reference to accompanying drawing and example, the present invention is further described, wherein:
Fig. 1 is equipment schematic 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 the system of real-time Transmission to be applicable to analog machine land empty call environment simulation system with the use of, be configured in full dynamic simulated machine, form the simulator system of a complete simulated flight environment.This parameter acquisition realizes Real-time Collection flight parameter with transmission in all kinds of flight subject is trained, by the empty verbal system terminal in land according to relevant land sky call principle and mechanism, the audio frequency that intelligence generates various calls exports, the empty call voice environment in land of Reality simulation flight and scene.
See 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 controlled, and 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 in analog machine main frame and carries out data acquisition, and the information of collection sends to the empty call terminal in land to process by output module.System also comprises the empty verbal system main frame in land be connected by the empty call terminal in TCP/IP network and land, main frame is provided with control zone multi-dimensional database, this database is the Multidimensional Data Model maintenance data base of all kinds of blank pipe area control, be the data source of blank pipe region recognition, decision algorithm, comprise all kinds of blank pipe region and mass data.
As shown in the process flow diagram in Fig. 2, first system of the present invention carries out data, buffer zone and communication protocol initialization, activate the flight parameter acquisition module be embedded in full dynamic simulated machine, obtain analog machine BSD data, again standard, format conversion are carried out to the data gathered, generate communication data message, by TCP/IP network, supplemental characteristic is sent to the empty call terminal in land through transport module, the database finally calling end host carries out data processing.In addition, system of the present invention also has exception, error handle and warning, automatically repair mechanism, can enter automatic business processing in time when there is exception, mistake in parameter acquisition.
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 of collection sends to the empty call terminal in land by 10HZ frequency.Transport module is connected by the empty call terminal in TCP/IP network and land.
System of the present invention can on request needed for real-time acquisition system analog machine flight, state parameter, carry out standard, form mathematical operation conversion if desired, generate flight parameter data message, and press interval setup time by gathering the flight parameter data message generated, be sent to the empty verbal system/common apparatus in corresponding analog machine land and system main-control platform module by TCP/IP procotol.
System configuration of the present invention is on analog machine, Real-time Collection flight parameter is realized in all kinds of flight subject training, according to relevant land sky call principle and mechanism, the audio frequency that intelligence generates various calls exports, the empty call voice environment in land of Reality simulation flight and scene, and then meet the needs of high analogue simulation machine system, analog machine is played and replaces true civil aircraft to carry out normal subject and improper section object flight training effect, effective enhancement training quality and reduction training cost.
The above, just preferred embodiment of the present invention, 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 (3)
1. a Real-time Collection full dynamic simulated machine flight parameter the system of real-time Transmission, it is characterized in that: described system comprises the flight parameter acquisition module and transport module that are connected to each other, described flight parameter acquisition module is embedded in the analog machine main frame for the simulator system of flight environment of vehicle simulation, Real-time Collection flight parameter data in the process of analog machine simulated flight, the empty call terminal in the land flight parameter data of collection being sent to simulator system by network by described transport module processes; Described system also comprises abnormality processing and alarm module, can automatically repair in time and alert process during for gathering in flight parameter data procedures occur exception, mistake to described flight parameter acquisition module; Wherein, the flight parameter of described flight parameter acquisition module collection comprises airport code, runway code, radio altitude, aircraft transit square degree and air speed.
2. Real-time Collection according to claim 1 full dynamic simulated machine flight parameter the system of 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 of collection sends to the empty call terminal in land by 10HZ frequency.
3. Real-time Collection according to claim 1 full dynamic simulated machine flight parameter the system of real-time Transmission, is characterized in that, described transport module is connected by the empty call terminal of TCP/IP network and land.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310183855.8A CN103295447B (en) | 2013-05-17 | 2013-05-17 | A kind of Real-time Collection full dynamic simulated machine flight parameter the system of real-time Transmission |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310183855.8A CN103295447B (en) | 2013-05-17 | 2013-05-17 | A kind of Real-time Collection full dynamic simulated machine flight parameter the system of real-time Transmission |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103295447A CN103295447A (en) | 2013-09-11 |
| CN103295447B true CN103295447B (en) | 2015-11-04 |
Family
ID=49096229
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310183855.8A Active CN103295447B (en) | 2013-05-17 | 2013-05-17 | A kind of Real-time Collection full dynamic simulated machine flight parameter the system of real-time Transmission |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103295447B (en) |
Families Citing this family (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 |
| 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 |
| CN114638442B (en) * | 2022-05-19 | 2022-09-02 | 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 |
| 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 |
| 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 |
| 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 |
| 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 |
| 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 |
| CN102053563A (en) * | 2010-12-27 | 2011-05-11 | 刘宇 | Flight training data acquisition and quality evaluation system of analog machine |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103295447A (en) | 2013-09-11 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103295447B (en) | A kind of Real-time Collection full dynamic simulated machine flight parameter the system of real-time Transmission | |
| CN202533754U (en) | Ground monitoring system for unmanned vehicle physical simulated test platform | |
| MX2020001767A (en) | An unmanned aerial vehicle system for inspecting railroad assets. | |
| CN106716973A (en) | Control method and ground control terminal of unmanned aerial vehicle | |
| CN105573336A (en) | Portable ground station capable of supporting multiple unmanned aerial vehicles | |
| CN203786910U (en) | Beidou low-altitude flight monitoring system | |
| CN105487409B (en) | Unmanned plane spatial domain integrated flight security management and control demonstration and verification platform | |
| CN105976672A (en) | Multifunctional flight teaching platform | |
| CN110278023A (en) | A kind of application system and method based on vacant lot broadband connections | |
| CN105427704A (en) | Use and maintenance simulator oriented to unmanned aerial vehicle flight control and task system | |
| CN106652631A (en) | Airport operation control simulation training device | |
| CN105182874A (en) | Real-time flight state monitoring system based on returned flight data, and method | |
| CN104076820A (en) | Unmanned aerial vehicle electric power line polling control system and method based on three-dimensional GIS | |
| CN101739859A (en) | Scene surveillance radar simulation system | |
| CN109116864A (en) | A kind of unmanned plane cluster terrestrial information acquisition identification management method | |
| CN106066649A (en) | Information for aircraft transmits the method and system with information sharing | |
| CN111343287B (en) | Helicopter laser radar remote monitoring system and method for power transmission line inspection | |
| CN105487518B (en) | Four axis UAV Flight Control Systems | |
| CN108762225A (en) | A kind of failure in flight control system copes with decision making device | |
| CN107256032A (en) | Unmanned plane large-range monitoring application process | |
| CN104091471A (en) | Monitoring control terminal and monitoring control communication method and system of track target | |
| CN204498275U (en) | The patrol unmanned machine of a kind of optimizing data | |
| US20150257080A1 (en) | Electronic interface between communication networks among vehicles | |
| CN103310783B (en) | For phonetic synthesis/integration method and the system of the empty call environment in analog machine land | |
| CN104168393B (en) | A kind of voice scheduling method for generating the empty call voice content in optimal land |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |