CN104503259A - Universal programmable aircraft simulator system for launch control system - Google Patents
Universal programmable aircraft simulator system for launch control system Download PDFInfo
- Publication number
- CN104503259A CN104503259A CN201410707505.1A CN201410707505A CN104503259A CN 104503259 A CN104503259 A CN 104503259A CN 201410707505 A CN201410707505 A CN 201410707505A CN 104503259 A CN104503259 A CN 104503259A
- Authority
- CN
- China
- Prior art keywords
- module
- signal
- control system
- interface
- communication
- 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.)
- Pending
Links
Landscapes
- Programmable Controllers (AREA)
- Testing And Monitoring For Control Systems (AREA)
- Debugging And Monitoring (AREA)
Abstract
The invention relates to a universal programmable aircraft simulator system for a launch control system, and belongs to the technical field of aircraft simulation. The system aims at solving the problems that a conventional simulator is achieved through pure hardware circuits, and is poorer in universality and flexibility. The interior of a controller module is provided with a simulator module in a preset manner, and the simulator module operates in the controller module and used for achieving the programmable core control of a simulator. An interface module is used for achieving the commination signal transmission between the controller module and a single-conditioning module. The single-conditioning module is used for the isolation and conditioning of analog and digital signals inputted from the outside, and also used for signal transmission. A display output module is used for receiving and displaying a signal transmitted by the single-conditioning module, and also used for transmitting a control signal inputted from the outside to the single-conditioning module. The system serves as an aircraft simulator.
Description
Technical field
The present invention relates to launching control system general programmable Flight Simulator system, belong to aircraft simulation technical field.
Background technology
Launching control system is the important component part of armament systems, and primary responsibility completes aircraft and penetrates the work such as front detection, parameter bookbinding and emission process control.The quality of its function and performance can directly affect armament systems result of use and fighting efficiency.
Flight Simulator is the important component devices of launching control system, under the mode of operation such as test maintaining and training, usually uses Flight Simulator to substitute aircraft and carries out the test maintaining of system, localization of fault or simulated training.In addition, also by Flight Simulator, simulated failure is set to check the troubleshooting capability of launching control system, improves reliability and the security of launching control system design.Flight Simulator generally adopted pure hardware circuit to realize in the past, its versatility and dirigibility poor, after board design is produced, generally cannot change its steering logic, and panel adopt pilot lamp instruction, man-machine interaction effect is friendly not.
Summary of the invention
The present invention seeks to adopt pure hardware circuit to realize to solve existing Flight Simulator, versatility and the poor problem of dirigibility, provide a kind of launching control system general programmable Flight Simulator system.
Launching control system general programmable Flight Simulator system of the present invention, it comprises controller module, interface module, Signal-regulated kinase and display translation module,
Controller module internal preset puts emulation module, and emulation module is run in controller module, controls for realizing the programmable core of simulator;
Interface module is for realizing the signal of communication transmission between controller module and Signal-regulated kinase;
Signal-regulated kinase is used for carrying out isolate to the analog quantity of outside input and digital quantity signal and nursing one's health, and carries out the transmission of signal;
Display translation module is used for the signal of Received signal strength conditioning module transfer and shows, and sends the control signal of outside input to Signal-regulated kinase simultaneously.
It also comprises power module,
Power module is used for providing working power, the DC/DC electric power generating composition that power module is inputted by multichannel 27V for controller module, interface module, Signal-regulated kinase and display translation module.
Described interface module comprises I/O module, A/D module and communication module,
I/O module adopts light-coupled isolation to its input signal received, and 27V signal is transformed into Transistor-Transistor Logic level signal, adopts light-coupled isolation or optical relay driving circuit output signal, realizes the transmission of signal;
A/D module adopts both-end isolation and multidiameter option switch and analog to digital conversion circuit process the signal received and realize the transmission of signal;
Communication module adopts FPGA+IP to examine existing standard HDLC 422 synchronous communication circuit, to carry out interface signal transmission.
Controller module selection standard PC104 mainboard module realizes.
Signal-regulated kinase is nursed one's health analog quantity by dividing potential drop buffer circuit, sends out flow control journey, by the load of high-power resistance analog power and priming system load by sequential circuit simulation.
Display translation module, by front panel display screen display Received signal strength, carries out the input and output of signal of communication by back panel connector.
Described emulation module completes the electric interface emulates of aircraft by number connect test; When receiving digital quantity input signal, perform corresponding actions by switching value output signal and show executing state on interface; By analog input sampling, quantitative test is carried out to analog quantity, measurement data result is presented on interface; By communication interface and launching control system communication, realize communication simulation function; And simulated failure state is set, coordinate launching control system to complete fault mode debugging.
Advantage of the present invention: the present invention is used for realizing Flight Simulator design, and it, by the combination of computer technology, peripheral signal processing circuit and interface board, achieves the PLC technology of Flight Simulator.What it made different model differ greatly sends out the versatility reinforcement controlling Flight Simulator hardware platform, and has more dirigibility.
Accompanying drawing explanation
Fig. 1 is the theory diagram of launching control system general programmable Flight Simulator system of the present invention.
Embodiment
Embodiment one: present embodiment is described below in conjunction with Fig. 1, the general programmable Flight Simulator system of launching control system described in present embodiment, it comprises controller module 1, interface module 2, Signal-regulated kinase 3 and display translation module 4,
Controller module 1 internal preset puts emulation module, and emulation module is run in controller module 1, controls for realizing the programmable core of simulator;
Interface module 2 is for realizing the signal of communication transmission between controller module 1 and Signal-regulated kinase 3;
Signal-regulated kinase 3 carries out isolating for the analog quantity that inputs outside and digital quantity signal and nurses one's health, and carries out the transmission of signal;
Display translation module 4 is nursed one's health the signal of module 3 transmission for Received signal strength and is shown, and sends the control signal of outside input to Signal-regulated kinase 3 simultaneously.
Present embodiment constructs able to programme control Flight Simulator system.
Embodiment two: present embodiment is described below in conjunction with Fig. 1, present embodiment is described further embodiment one, and it also comprises power module 5,
Power module 5 is for providing working power for controller module 1, interface module 2, Signal-regulated kinase 3 and display translation module 4, the DC/DC electric power generating composition that power module 5 is inputted by multichannel 27V.
Power module 5 can provide the various voltages needed for each module.
Embodiment three: present embodiment is described further embodiment one or two, described interface module 2 comprises I/O module, A/D module and communication module,
I/O module adopts light-coupled isolation to its input signal received, and 27V signal is transformed into Transistor-Transistor Logic level signal, adopts light-coupled isolation or optical relay driving circuit output signal, realizes the transmission of signal;
A/D module adopts both-end isolation and multidiameter option switch and analog to digital conversion circuit process the signal received and realize the transmission of signal;
Communication module adopts FPGA+IP to examine existing standard HDLC 422 synchronous communication circuit, to carry out interface signal transmission.
Embodiment four: present embodiment is described further embodiment one, two or three, controller module 1 selection standard PC104 mainboard module realizes.
Embodiment five: present embodiment is described further embodiment one, two, three or four, Signal-regulated kinase 3 is nursed one's health analog quantity by dividing potential drop buffer circuit, flow control journey is sent out, by the load of high-power resistance analog power and priming system load by sequential circuit simulation.
Embodiment six: present embodiment is described further embodiment one, two, three, four or five, display translation module 4, by front panel display screen display Received signal strength, carries out the input and output of signal of communication by back panel connector.
Embodiment seven: present embodiment is described below in conjunction with Fig. 1, present embodiment is described further embodiment one, two, three, four, five or six, and described emulation module completes the electric interface emulates of aircraft by number connect test; When receiving digital quantity input signal, perform corresponding actions by switching value output signal and show executing state on interface; By analog input sampling, quantitative test is carried out to analog quantity, measurement data result is presented on interface; By communication interface and launching control system communication, realize communication simulation function; And simulated failure state is set, coordinate launching control system to complete fault mode debugging.
Present invention achieves the software programmable configuration of Flight Simulator functional module, different model launching control system demand can be adapted to.
Claims (7)
1. a launching control system general programmable Flight Simulator system, is characterized in that, it comprises controller module (1), interface module (2), Signal-regulated kinase (3) and display translation module (4),
Controller module (1) internal preset puts emulation module, and emulation module is run in controller module (1), controls for realizing the programmable core of simulator;
Interface module (2) is for realizing the signal of communication transmission between controller module (1) and Signal-regulated kinase (3);
Signal-regulated kinase (3) carries out isolating for the analog quantity that inputs outside and digital quantity signal and nurses one's health, and carries out the transmission of signal;
Display translation module (4) is for Received signal strength conditioning module (3) signal that transmits and show, and sends the control signal of outside input to Signal-regulated kinase (3) simultaneously.
2. launching control system general programmable Flight Simulator system according to claim 1, it is characterized in that, it also comprises power module (5),
Power module (5) is for providing working power, the DC/DC electric power generating composition that power module (5) is inputted by multichannel 27V for controller module (1), interface module (2), Signal-regulated kinase (3) and display translation module (4).
3. launching control system general programmable Flight Simulator system according to claim 2, is characterized in that,
Described interface module (2) comprises I/O module, A/D module and communication module,
I/O module adopts light-coupled isolation to its input signal received, and 27V signal is transformed into Transistor-Transistor Logic level signal, adopts light-coupled isolation or optical relay driving circuit output signal, realizes the transmission of signal;
A/D module adopts both-end isolation and multidiameter option switch and analog to digital conversion circuit process the signal received and realize the transmission of signal;
Communication module adopts FPGA+IP to examine existing standard HDLC 422 synchronous communication circuit, to carry out interface signal transmission.
4. launching control system general programmable Flight Simulator system according to claim 3, is characterized in that, controller module (1) selection standard PC104 mainboard module realizes.
5. launching control system general programmable Flight Simulator system according to claim 4, it is characterized in that, Signal-regulated kinase (3) is nursed one's health analog quantity by dividing potential drop buffer circuit, flow control journey is sent out, by the load of high-power resistance analog power and priming system load by sequential circuit simulation.
6. launching control system general programmable Flight Simulator system according to claim 5, it is characterized in that, display translation module (4), by front panel display screen display Received signal strength, carries out the input and output of signal of communication by back panel connector.
7. the general programmable Flight Simulator system of the launching control system according to claim 1,2,3,4,5 or 6, is characterized in that, described emulation module completes the electric interface emulates of aircraft by number connect test; When receiving digital quantity input signal, perform corresponding actions by switching value output signal and show executing state on interface; By analog input sampling, quantitative test is carried out to analog quantity, measurement data result is presented on interface; By communication interface and launching control system communication, realize communication simulation function; And simulated failure state is set, coordinate launching control system to complete fault mode debugging.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410707505.1A CN104503259A (en) | 2014-11-27 | 2014-11-27 | Universal programmable aircraft simulator system for launch control system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410707505.1A CN104503259A (en) | 2014-11-27 | 2014-11-27 | Universal programmable aircraft simulator system for launch control system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104503259A true CN104503259A (en) | 2015-04-08 |
Family
ID=52944663
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410707505.1A Pending CN104503259A (en) | 2014-11-27 | 2014-11-27 | Universal programmable aircraft simulator system for launch control system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104503259A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105974824A (en) * | 2016-01-15 | 2016-09-28 | 中测新图(北京)遥感技术有限责任公司 | Universal control system of digital aerial photography system |
| CN106647331A (en) * | 2016-12-28 | 2017-05-10 | 中国航空工业集团公司西安飞机设计研究所 | Engineering simulator comprehensive control system |
| CN107219842A (en) * | 2017-05-31 | 2017-09-29 | 北京电子工程总体研究所 | The activation control simulated testing system of priming system on a kind of aircraft |
| CN108891622A (en) * | 2018-06-22 | 2018-11-27 | 湖北三江航天红峰控制有限公司 | A kind of autonomous controllable universal test launching control system |
| CN111114826A (en) * | 2019-12-27 | 2020-05-08 | 中国航空工业集团公司沈阳飞机设计研究所 | Detection device for onboard control circuit of distributed fire control system |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101782754A (en) * | 2009-12-30 | 2010-07-21 | 北京宇航系统工程研究所 | Redundancy switching circuit used for ground test launch and control system of carrier rocket |
| CN102495646A (en) * | 2011-12-02 | 2012-06-13 | 哈尔滨工业大学 | Flywheel simulator with reconfigurable function |
| EP2618099A2 (en) * | 2012-01-17 | 2013-07-24 | MBDA Deutschland GmbH | Test and test device for a missile launching device and method for testing and/or testing the functionality of a missile launching device |
| CN104049687A (en) * | 2014-05-27 | 2014-09-17 | 上海微小卫星工程中心 | Embedded cubic star task computer based on FPGA (Field Programmable Gate Array) and reconstruction method thereof |
| CN104113371A (en) * | 2014-07-23 | 2014-10-22 | 成都天奥信息科技有限公司 | Transmit type satellite monitoring simulating device and working and application method |
-
2014
- 2014-11-27 CN CN201410707505.1A patent/CN104503259A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101782754A (en) * | 2009-12-30 | 2010-07-21 | 北京宇航系统工程研究所 | Redundancy switching circuit used for ground test launch and control system of carrier rocket |
| CN102495646A (en) * | 2011-12-02 | 2012-06-13 | 哈尔滨工业大学 | Flywheel simulator with reconfigurable function |
| EP2618099A2 (en) * | 2012-01-17 | 2013-07-24 | MBDA Deutschland GmbH | Test and test device for a missile launching device and method for testing and/or testing the functionality of a missile launching device |
| CN104049687A (en) * | 2014-05-27 | 2014-09-17 | 上海微小卫星工程中心 | Embedded cubic star task computer based on FPGA (Field Programmable Gate Array) and reconstruction method thereof |
| CN104113371A (en) * | 2014-07-23 | 2014-10-22 | 成都天奥信息科技有限公司 | Transmit type satellite monitoring simulating device and working and application method |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105974824A (en) * | 2016-01-15 | 2016-09-28 | 中测新图(北京)遥感技术有限责任公司 | Universal control system of digital aerial photography system |
| CN106647331A (en) * | 2016-12-28 | 2017-05-10 | 中国航空工业集团公司西安飞机设计研究所 | Engineering simulator comprehensive control system |
| CN107219842A (en) * | 2017-05-31 | 2017-09-29 | 北京电子工程总体研究所 | The activation control simulated testing system of priming system on a kind of aircraft |
| CN108891622A (en) * | 2018-06-22 | 2018-11-27 | 湖北三江航天红峰控制有限公司 | A kind of autonomous controllable universal test launching control system |
| CN111114826A (en) * | 2019-12-27 | 2020-05-08 | 中国航空工业集团公司沈阳飞机设计研究所 | Detection device for onboard control circuit of distributed fire control system |
| CN111114826B (en) * | 2019-12-27 | 2023-03-14 | 中国航空工业集团公司沈阳飞机设计研究所 | Detection device for onboard control circuit of distributed fire control system |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104503259A (en) | Universal programmable aircraft simulator system for launch control system | |
| CN103925853B (en) | A kind of carrier rocket ground testing system device | |
| CN106776188B (en) | Bus fault injection system based on DSP and FPGA | |
| CN106773787A (en) | A kind of unmanned plane during flying simulation demo verification platform based on serial communication | |
| CN206243509U (en) | A kind of analogue means of aircraft test signal | |
| CN203608196U (en) | 4M-transmission-rate 1553B bus cable test system | |
| CN205301911U (en) | Embedded fault injection control system | |
| CN106991001A (en) | Radionavigation recognizes simulation system | |
| CN110060541A (en) | A kind of aircraft navigation attitude equipment simulating training system | |
| CN201575752U (en) | Carrier rocket launch control console based on MODBUS/TCP protocol | |
| CN103021220B (en) | Railway station signal equipment simulation training system | |
| CN203013017U (en) | Distributed-type non-avionic simulation excitation system | |
| CN204480512U (en) | A kind of Armored Vehicle Driving person's terminal emulator | |
| CN116192716A (en) | ZYNQ-based avionics multi-protocol bus test platform | |
| CN104575157A (en) | Touching-type simulator for store management system | |
| CN104199776B (en) | Two multiply two test platforms for taking two vehicle-mounted softwares | |
| CN210006254U (en) | simulation training device for airplane attitude and heading system | |
| CN202075919U (en) | Serial bus experimental device | |
| CN204582551U (en) | The relay of aircraft remote control system | |
| CN101308195A (en) | High -voltage switch secondary circuit signal emulation system | |
| CN203759915U (en) | System used for simulating bridge operation | |
| CN110844114A (en) | Portable aerostat test system | |
| CN202126902U (en) | Resistance device with adjustable digital quantity | |
| CN206147979U (en) | Comprehensive test simulation training system | |
| CN209928240U (en) | Remote control system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20150408 |