Aircraft wireless test launch control system and method

A technology for launch control and wireless testing, applied in aircraft component testing, transmission systems, instruments, etc., can solve the problems of a large number of wires and cables, manpower, material resources and time, saving laying manpower, shortening launch preparation time, and improving Testing the Effects of Launch Control Efficiency

Active Publication Date: 2022-05-13
THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

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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  • Aircraft wireless test launch control system and method
  • Aircraft wireless test launch control system and method
  • Aircraft wireless test launch control system and method

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Embodiment Construction

[0032] The present invention will be described in further detail below in conjunction with the accompanying drawings and embodiments.

[0033] see figure 1 As shown, the embodiment of the present invention provides a wireless test launch control system for an aircraft, including: a ground device and an aircraft device.

[0034] The ground device is provided with a first communication component and an electric energy transmitting component. The aircraft device is provided with a second communication component and a power receiving component. The second communication component is used to wirelessly receive the test launch control command of the first communication component of the ground device and transmit it to other equipment of the aircraft device. The other devices of the aircraft device transmit according to the test. The control command completes the autonomous test emission control and forms the test emission control result, and the second communication component wirele...

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Abstract

The invention discloses a wireless test launch control system and method for an aircraft, and relates to the field of aerospace test launch control. The system includes: a ground device and an aircraft device, the ground device is provided with a first communication component and an electric energy transmitting component; the aircraft device is provided with The second communication component and the power receiving component, the second communication component is used to wirelessly receive the test launch control command of the first communication component of the ground device, and transmit it to other equipment of the aircraft device; the other equipment of the aircraft device is controlled according to the test launch The command completes the autonomous test emission control and forms the test emission control result, and the second communication component wirelessly sends the test emission result to the first communication component; the power receiving component is used for wirelessly receiving the power of the power transmitting component. The invention can solve the problem that the existing test launch control system and method adopt wired connection, have a large number of wires and cables, and consume manpower, material resources and time.

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...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H04B17/00B64F5/60G01R31/00
CPCH04B17/00H04B17/0085B64F5/60G01R31/00
Inventor 宋长哲谢扬张红吴翔李朝波王卓杜鹏王立
Owner THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD
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