Spacecraft on-orbit space debris collision multi-parameter detection system and detection method

A technology of space debris and detection system, which is applied in the detection of collision multi-parameters and the detection device of multi-parameter collision of spacecraft on-orbit space debris, can solve the problems of difficulty in key parameters such as speed, direction and size of space debris, and achieve the prevention of two The effect of secondary destruction, high precision and high sensitivity

Active Publication Date: 2021-10-08
BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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Problems solved by technology

[0009] Aiming at the problem that key parameters such as speed, direction and size of space debris in the operating environment of spacecraft are difficult to measure and obtain, the present invention proposes a multi-parameter detection method for space debris impact

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  • Spacecraft on-orbit space debris collision multi-parameter detection system and detection method
  • Spacecraft on-orbit space debris collision multi-parameter detection system and detection method
  • Spacecraft on-orbit space debris collision multi-parameter detection system and detection method

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Embodiment Construction

[0080] The following introduces the specific implementation mode as the content of the present invention, and the content of the present invention will be further clarified through the specific implementation mode below. Of course, the following specific embodiments are described only to illustrate different aspects of the present invention, and should not be construed as limiting the scope of the present invention.

[0081] see figure 1 , figure 1 It is a structural schematic diagram of a space debris key parameter detection system of a capacitive array of the present invention; it includes a capacitive array film, a metal plate, a fixed bracket, a PVDF piezoelectric sensor, an ultrasonic sensor, a multi-channel scanning capacitive reactance detection module, and a preamplification module , signal acquisition module, signal excitation module and computer, the capacitor array film and the metal plate are installed in parallel through a fixed bracket, and the two are kept at a...

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Abstract

The invention discloses a multi-parameter detection system and detection method based on spacecraft on-orbit space debris collision, wherein the debris collides with a capacitor array film and a metal plate to form an elastic wave, which is obtained by detecting the amplified signal of the capacitance and the elastic wave parameters to calculate the corresponding parameters for various fragments. The invention also discloses a corresponding detection method for key parameters of space debris. The invention can detect parameters such as fragment size, speed, flight direction, collision position, etc., and has the characteristics of higher sensitivity, and the accuracy of measurement results is higher, and the detection sensitivity can reach 0.1mm.

Description

technical field [0001] The invention belongs to the technical field of spacecraft structural health parameter detection. Specifically, the invention relates to a multi-parameter detection device for collision of space debris in orbit of a spacecraft, and also relates to a multi-parameter detection method for collision. Background technique [0002] With the continuous development of the aerospace industry of various countries, the number of debris in the space field is increasing day by day. The existence of these debris directly threatens the safe operation of spacecraft in orbit. Although after years of technological development, the protective materials and protective structure design of the spacecraft have been greatly improved, which can effectively protect small-volume debris, but the protection effect on centimeter-level or even millimeter-level debris is limited. Real-time monitoring is carried out to obtain parameters such as debris size, speed, flight direction, an...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01M7/08B64G1/66
CPCB64G1/66G01M7/08
Inventor 綦磊孙立臣崔寓淏芮小博孟冬辉张景川孙伟冯咬齐赵越阳
Owner BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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