Aircraft and ground cooperative test launch control system and control method

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...

AI Technical Summary

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 problems of the related technologies in which the ground measurement and control system has a large number of equipment and a complex structure, which causes the operation Complicated and inconvenient maintenance

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