Aircraft and ground cooperative test launch control system and control method

A technology of measurement, launch and control system and aircraft, which is applied in aircraft component testing, electrical program control, program control in sequence/logic controllers, etc., can solve problems such as inconvenient maintenance, complex structure, and complicated operation, and achieve lightweight The effect of portability and reduction of operational complexity

Inactive Publication Date: 2021-03-26
THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD
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  • Claims
  • Application Information

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Problems solved by technology

[0004] Aiming at one of the defects existing in the prior art, the purpose of this application is to provide an aircraft and ground cooperative measurement and control system and control method to solve the ...

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  • Aircraft and ground cooperative test launch control system and control method
  • Aircraft and ground cooperative test launch control system and control method
  • Aircraft and ground cooperative test launch control system and control method

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Embodiment Construction

[0048] In order to make the purpose, technical solution and advantages of the present application clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention. In addition, the technical features involved in the various embodiments of the present invention described below can be combined with each other as long as they do not constitute a conflict with each other.

[0049] Embodiments of the present application provide an aircraft-ground cooperative measurement and launch control system and a control method, which can solve the problems of cumbersome test operations and inconvenient maintenance due to the large number of equipment and complex structure of the ground measurement and launch control system.

[0050] Such as figure 1 As shown, the aircraft ...

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Abstract

The invention discloses an aircraft and ground cooperative test launch control system and control method, and relates to the technical field of aircraft test launch control. The system comprises a remote launching controller which is used for generating a third control instruction for controlling the launching of an aircraft, a ruggedized computer which is used for sending a first control instruction and a second control instruction, and forwarding the third control instruction generated by the remote launching controller to a test-launch-control all-in-one machine, a ground power supply whichis used for supplying power to the test-launch-control all-in-one machine, and the test-launch-control all-in-one machine is used for sending a test instruction to other equipment on the aircraft andsending obtained test data to the ruggedized computer; and when the ruggedized computer judges that the test data are normal, the test-launch-control all-in-one machine is further used for carrying out launch control on the aircraft. According to the invention, an integrated aircraft and ground cooperative test launch control architecture which takes tests on the aircraft as a main part and takesground tests as an auxiliary part is constructed, so that overall miniaturization, light weight and portability are realized, and the operation complexity and the use and maintenance cost of the system are reduced.

Description

technical field [0001] This application relates to the technical field of aircraft measurement and launch control, and in particular to an aircraft and ground cooperative measurement and launch control system and control method. Background technique [0002] At present, the aircraft test and launch control system is responsible for testing the performance of the aircraft and launching control. In the related technology, the ground measurement, transmission and control is mainly composed of a measurement and control host, a launch and control host, a display, a ground power supply, and a cable network. The measurement and control host mainly realizes the measurement of voltage, switch, and status indication signals on the ground and the aircraft; the launch and control host mainly implements the control when the aircraft is launched, such as power distribution to the aircraft, status switching control of the aircraft safety control mechanism, and thermal battery activation. D...

Claims

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Application Information

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IPC IPC(8): B64F5/60B64F1/04H04W4/44H02J9/06G05B19/04
CPCB64F5/60B64F1/04H04W4/44H02J9/068G05B19/04
Inventor 席茂军熊朝羽宋长哲丁波王卓李冰陈芳艾迪储敏
Owner THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD
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