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Universal programmable aircraft simulator system for launch control system

A simulator and aircraft technology, applied in the field of aircraft simulation, can solve problems such as poor versatility and flexibility, and achieve the effect of more flexibility and enhanced versatility

Inactive Publication Date: 2015-04-08
BEIJING INST OF ELECTRONICS SYST ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to solve the problem that the existing aircraft simulators are implemented by pure hardware circuits, and the versatility and flexibility are poor, and a general programmable aircraft simulator system for launch control systems is provided.

Method used

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  • Universal programmable aircraft simulator system for launch control system

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specific Embodiment approach 1

[0022] Specific implementation mode one: the following combination figure 1 Describe the present embodiment, the launch control system described in the present embodiment uses a general programmable aircraft simulator system, which includes a controller module 1, an interface module 2, a signal conditioning module 3 and a display output module 4,

[0023] The simulator module is preset inside the controller module 1, and the simulator module runs in the controller module 1 to realize the programmable core control of the simulator;

[0024] The interface module 2 is used to realize the communication signal transmission between the controller module 1 and the signal conditioning module 3;

[0025] The signal conditioning module 3 is used for isolating and conditioning externally input analog and digital signals, and transmitting the signals;

[0026] The display output module 4 is used for receiving the signal transmitted by the signal conditioning module 3 and displaying it, a...

specific Embodiment approach 2

[0028] Specific implementation mode two: the following combination figure 1 This embodiment will be described. This embodiment will further describe the first embodiment, which also includes a power supply module 5,

[0029] The power supply module 5 is used to provide working power for the controller module 1, the interface module 2, the signal conditioning module 3 and the display output module 4. The power supply module 5 is composed of multiple 27V input DC / DC power supplies.

[0030] The power supply module 5 can provide various voltages required by each module.

specific Embodiment approach 3

[0031] Specific implementation mode three: this implementation mode further explains the first or second implementation mode, the interface module 2 includes an I / O module, an A / D module and a communication module,

[0032] The I / O module uses optocoupler isolation for the input signal it receives, converts the 27V signal into a TTL level signal, and uses optocoupler isolation or photorelay drive circuit to output the signal to realize signal transmission;

[0033] The A / D module uses double-ended isolation, multi-channel selection switch and analog-to-digital conversion circuit to process the received signal and realize the signal transmission;

[0034] The communication module uses FPGA+IP core to realize the standard HDLC 422 synchronous communication circuit for interface signal transmission.

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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 [0001] The invention relates to a general programmable aircraft simulator system for a launch control system, belonging to the technical field of aircraft simulation. Background technique [0002] The launch control system is an important part of the weapon system. It is mainly responsible for the pre-launch detection of the aircraft, parameter binding, and launch process control. Its function and performance will directly affect the use effect and combat effectiveness of the weapon system. [0003] The aircraft simulator is an important component of the launch control system. In the working mode of test maintenance and training, the aircraft simulator is usually used instead of the aircraft for system test maintenance, fault location or simulation training. In addition, the fault handling capability of the launch control system can also be tested by setting simulated faults in the aircraft simulator, and the reliability and safety of the launch control syst...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B17/02
Inventor 程鹏田福强王玉姣邓昕才
Owner BEIJING INST OF ELECTRONICS SYST ENG
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