Wireless test emission control system and method for aircraft

Abstract

The invention discloses a wireless test emission control system and method for an aircraft, and relates to the field of spaceflight test emission control, the system comprises a ground device and an aircraft device, and the ground device is provided with a first communication assembly and an electric energy emission assembly; the aircraft device is provided with a second communication assembly andan electric energy receiving assembly, and the second communication assembly is used for wirelessly receiving a test emission control instruction of the first communication assembly of the ground device and transmitting the test emission control instruction to other equipment of the aircraft device; other equipment of the aircraft device completes autonomous test emission control according to thetest emission control instruction and forms a test emission control result, and the second communication assembly wirelessly sends the test emission result to the first communication assembly; and the electric energy receiving assembly is used for wirelessly receiving the electric energy of the electric energy transmitting assembly. According to the invention, the problems that the existing testemission control system and method adopt wired connection, the number of wires and cables is large, and manpower, material resources and time are consumed can be solved.

Description

technical field [0001] The invention relates to the technical field of aerospace test launch control, in particular to a wireless test launch control system and method for an aircraft. Background technique [0002] The test launch control system of an aircraft generally includes ground equipment and aircraft equipment. At present, most ground equipment and aircraft equipment are connected by wires and cables to realize communication and power transmission between the two. [0003] Test launch control systems based on wired connections suffer from the following problems: [0004] First, the number of wires and cables in the system is large, the quality is large, and the connection relationship is complicated. Special wire and cable laying work is required at the launch site of the aircraft, which is highly dependent on human resources, which increases the complexity of the system, reduces the portability of the system, and increases the reliability of the aircraft. launch pr...

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Problems solved by technology

[0006] Aiming at the defects existing in the prior art, the object of the present invention is to provide a wireless test launch control system and method for an aircraft, which is used to solve the existing test launch control system and method, adopts wired connection, and has a large number of wires and cables, which consumes Manpower, material resources and time issues

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