Volume 43 Issue 12
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Wang Weibing, Jiang Zhenhua, Wang Tingfeng, Guo Jin. Opto-electrical compound axis tracking control technology on satellite[J]. Infrared and Laser Engineering, 2014, 43(12): 4133-4139.
Citation: Wang Weibing, Jiang Zhenhua, Wang Tingfeng, Guo Jin. Opto-electrical compound axis tracking control technology on satellite[J]. Infrared and Laser Engineering, 2014, 43(12): 4133-4139.

Opto-electrical compound axis tracking control technology on satellite

  • Received Date: 2014-04-04
  • Rev Recd Date: 2014-05-20
  • Publish Date: 2014-12-25
  • It's becoming a research hot topic that two axis opto-electrical tracking instrument is loaded on satellite to continuously track and observe moving target in space. At present, there are Space-Based Space Surveillance System (SBSS), Space Tracking and Surveillance System (STSS) and Precision Tracking and Surveillance System (PTSS). In order to deal with stable tracking control technology for opto-electrical axis on the condition of dynamic platform on satellite, firstly, simplifying physics model of opto-electrical tracking control system on satellite. Secondly, solving relative angular velocity and acceleration between two satellites near sun-synchronous orbits. Thirdly, analyzing active stable tracking control scheme and principle based on opto-electrical compound axis tracking control system. Lastly, establishing simulation model of opto-electrical compound axis tracking control system on satellite. And the results show that stable tracking precision is 2.5 for space object in the relative maneuvering range of (37.68 ()/s、47.33 ()/s) and space satellite that relative low velocity is 0.1 ()/s.
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Opto-electrical compound axis tracking control technology on satellite

  • 1. State Key Laboratory of Laser Interaction with Matter,Changchun Institute of Optics,Fine Mechanics and Physics,Chinese Academy of Science,Changchun 130033,China

Abstract: It's becoming a research hot topic that two axis opto-electrical tracking instrument is loaded on satellite to continuously track and observe moving target in space. At present, there are Space-Based Space Surveillance System (SBSS), Space Tracking and Surveillance System (STSS) and Precision Tracking and Surveillance System (PTSS). In order to deal with stable tracking control technology for opto-electrical axis on the condition of dynamic platform on satellite, firstly, simplifying physics model of opto-electrical tracking control system on satellite. Secondly, solving relative angular velocity and acceleration between two satellites near sun-synchronous orbits. Thirdly, analyzing active stable tracking control scheme and principle based on opto-electrical compound axis tracking control system. Lastly, establishing simulation model of opto-electrical compound axis tracking control system on satellite. And the results show that stable tracking precision is 2.5 for space object in the relative maneuvering range of (37.68 ()/s、47.33 ()/s) and space satellite that relative low velocity is 0.1 ()/s.

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