Ground test verification method and system for tethered drag control

A towing control and ground test technology, applied in the field of tethered towing, can solve problems such as threatening the safety of spacecraft operating in orbit and occupying orbital resources, and achieve the effect of true, credible, reliable and effective test data.

Active Publication Date: 2021-12-07
SHANGHAI AEROSPACE CONTROL TECH INST
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Problems solved by technology

These space debris occupy precious orbital resources and seriously threaten the safety of orbiting spacecraft

Method used

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  • Ground test verification method and system for tethered drag control
  • Ground test verification method and system for tethered drag control
  • Ground test verification method and system for tethered drag control

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Embodiment Construction

[0031] by reading reference Figure 1-Figure 4 The features, objects and advantages of the present invention will become more apparent from the detailed description of non-limiting examples. See the illustration of an embodiment of the invention Figure 1-Figure 4 , the present invention will be described in more detail below. However, this invention may be embodied in many different forms and should not be construed as limited to the embodiments set forth herein.

[0032] Such as figure 1 with figure 2 As shown, the present invention provides a ground test system for tether dragging control, including an active star simulator 1, a target star simulator 2, a tether retractable device 5, a dual six-degree-of-freedom platform motion control system, a GNC computer, Dynamics simulator, target control upper computer and target control lower computer. Wherein, the master console in the figure is composed of the GNC computer, the dynamics simulator and the target control host c...

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Abstract

The invention discloses a tether dragging control ground test verification method and system, which uses a dynamics simulation system to generate attitude and orbital motion data of a target star and an active star; uses the dynamics simulation system to output the position and attitude of the target star and the active star The information-driven dual six-degree-of-freedom motion simulation system generates the position and attitude movements of the target star simulator and the active star simulator; the pulling force of the tether on the target is obtained through the three-dimensional force sensor on the target star simulator, and the target star simulation is obtained through the gyroscope. The attitude information of the sailboard and the main body is transmitted to the dynamic simulation system. After conversion, the relative state information and the force information of the target star are sent to the GNC computer for drag control law calculation, and the control commands are sent to the active star. The tether retracting device on the simulator carries out the tether retracting and retracting control. The invention is used for the ground semi-physical closed-loop test of dragging removal control after the flying net capture of the invalid spacecraft, and provides technical support for the on-orbit obstacle removal service.

Description

technical field [0001] The invention relates to the field of tethered dragging, in particular to a method and system for testing and verifying ground movement controlled by tethered dragging. Background technique [0002] The application field of space technology has been rapidly expanded in the past one or two decades. In addition to the continuous deepening of space science applications, with the rapid development of space technology, more and more spacecraft have been launched into space. There are also more and more old spacecraft malfunctioning and becoming space debris. These space debris occupy precious orbital resources and seriously threaten the safety of orbiting spacecraft. [0003] Capturing targets by flying nets and dragging targets to deorbit orbits is an emerging solution to clean up space debris, and has received extensive attention and research due to its strong adaptability and reusability. [0004] After the rope net captures the target, the active star...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G09B23/08B64G7/00G01M99/00
CPCB64G7/00G01M99/005G01M99/008G09B23/08
Inventor 卢山刘禹徐晨詹鹏宇张竞天陈浩
Owner SHANGHAI AEROSPACE CONTROL TECH INST
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