Space non-cooperative target capture and control and assembly control test device and method

A non-cooperative target and control test technology, applied in the field of space non-cooperative target capture and manipulation and assembly control test equipment, can solve the problems of low robustness and real-time performance, and achieve strong engineering realization and good autonomy , The effect of simple principle

Active Publication Date: 2022-07-08
伸瑞科技(北京)有限公司 +1
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

However, the robustness and real-time performance of the method and system given by this scheme are not high, and it needs to be improved urgently.

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  • Space non-cooperative target capture and control and assembly control test device and method
  • Space non-cooperative target capture and control and assembly control test device and method
  • Space non-cooperative target capture and control and assembly control test device and method

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Embodiment Construction

[0025] The embodiments of the present invention will be described in detail below with reference to the accompanying drawings.

[0026] It should be noted that, the following embodiments and the features in the embodiments can be combined with each other without conflict; and, based on the embodiments in the present disclosure, those of ordinary skill in the art can obtain without creative work. All other embodiments of the present disclosure fall within the scope of protection of the present disclosure.

[0027] It is noted that various aspects of embodiments within the scope of the appended claims are described below. It should be apparent that the aspects described herein may be embodied in a wide variety of forms and that any specific structure and / or function described herein is illustrative only. Based on this disclosure, those skilled in the art should appreciate that an aspect described herein may be implemented independently of any other aspects and that two or more ...

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Abstract

The invention relates to the field of aircraft ground simulation, and provides a space non-cooperative target capture and control and assembly control test device and method, and the device comprises a simulation upper computer, a visual positioning system, a tracking star simulation system, and a target star simulation system. Wherein the simulation upper computer is used for sending a control instruction to the tracking star simulation system and / or the target star simulation system; the visual positioning system is used for acquiring pose information of the tracking star simulation system and / or the target star simulation system and feeding back the information to the tracking star simulation system and / or the target star simulation system; the tracking star simulation system is used for receiving a control instruction of the simulation upper computer, capturing the target star simulation system and measuring and calculating disturbance characteristics in the capturing process. The spatial non-cooperative target capture, control and assembly control test device is established, disturbance characteristics in the capture process can be calculated, assembly control can be achieved, problems in scheme design can be found, and algorithm performance can be analyzed and verified.

Description

technical field [0001] The invention relates to the field of aircraft ground simulation, in particular to a space non-cooperative target capture and manipulation and combined body control test device and method. Background technique [0002] With the rapid development of space technology, the utilization of space resources by human beings is also deepening, and the failed satellites in space orbit need to be repaired or removed. Due to these actual on-orbit service requirements, the capture and ground simulation of non-cooperative space targets Validation studies have important practical implications. [0003] Due to the special operating environment of the aircraft represented by satellites, the debugging and optimization of system operation control through the actual flight test of the prototype is costly, the cycle is long, and even difficult to achieve. Therefore, it is necessary to develop a relatively easy-to-implement low-cost and high-precision ground simulation syst...

Claims

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Application Information

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IPC IPC(8): G05B17/02
CPCG05B17/02Y02T90/00
Inventor 马广程马翌祥夏红伟王常虹李莉李同顺朱文山
Owner 伸瑞科技(北京)有限公司
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