A space non-cooperative target electromagnetic eddy current racemization capture device and method

A non-cooperative target, electromagnetic eddy current technology, used in transportation and packaging, space navigation equipment, space navigation aircraft, etc., can solve problems such as energy consumption, and achieve the effect of improving derotation efficiency, improving safety, and simplifying operation difficulty.

Active Publication Date: 2019-01-22
NORTHWESTERN POLYTECHNICAL UNIV
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  • Application Information

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  • A space non-cooperative target electromagnetic eddy current racemization capture device and method
  • A space non-cooperative target electromagnetic eddy current racemization capture device and method
  • A space non-cooperative target electromagnetic eddy current racemization capture device and method

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Embodiment Construction

[0039] In the description of the present invention, it should be understood that the orientation or positional relationship indicated by the terms "upper", "lower", "side", "one end", "side" etc. is based on the orientation or position shown in the drawings The relationship is only for the convenience of describing the present invention and simplifying the description, but does not indicate or imply that the referred device or element must have a specific orientation, be constructed and operated in a specific orientation, and thus should not be construed as a limitation of the present invention. In addition, in the description of the present invention, unless otherwise specified, "plurality" means two or more.

[0040] In the description of the present invention, it should be noted that unless otherwise specified and limited, the terms "installation", "connection" and "connection" should be understood in a broad sense, for example, it can be a fixed connection or a detachable c...

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Abstract

The invention discloses a space non-cooperative target electromagnetic eddy current racemization capture device and a method thereof. The device includes a working spacecraft equipped with solar panels; an observation system and a robotic arm are provided on the working spacecraft; the observing system is used to estimate the direction and speed of the target rotation, and the electromagnet is provided with an electromagnet for derotation; an end effector for capturing the target after the race is provided at the end of the robot arm. Compared with the small satellite formation-based race andcatch system, the present invention has advantages in control difficulty, fault tolerance and service life.

Description

technical field [0001] The invention belongs to the technical field of space non-cooperative target capture, and in particular relates to an electromagnetic eddy current spin-down capture device and method for space non-cooperative targets. Background technique [0002] Space non-cooperative target refers to any spacecraft that is not designed for docking or capture, that is, the target is not equipped with a gripping mechanism (handle) for robotic arm capture and cooperative markers and feature blocks for auxiliary measurement, or Any spacecraft that cannot perform attitude control and roll freely in space. Generally, it includes satellites without cooperative components installed by one’s own side and satellites with cooperative components installed by one’s own side but exhausted of fuel, satellites with malfunctioning attitude and orbit control systems, failed satellites of one’s own side, space debris, and the opponent’s spacecraft. Existing spacecraft in orbit are bas...

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Application Information

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IPC IPC(8): B64G1/66B64G4/00
CPCB64G1/66B64G4/00B64G2004/005
Inventor 袁建平彭志旺王明明王铮方静徐杨魏锦源李晨熹
Owner NORTHWESTERN POLYTECHNICAL UNIV
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