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Volume 31 Issue 03
Mar.  2005
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Journal of Beijing University of Aeronautics and Astronautics  > 2005  >  31(03): 265-269.
Ma Dianfu, Ge Sheng, Liu Xudonget al. WSDL presentation model and implementation method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2003, 29(10): 856-859. (in Chinese)
Citation: Dong Yunfeng, Xiao Yelun. Trajectory control logic of space exploration rocket required to arrive given site with zero speed at given time[J]. Journal of Beijing University of Aeronautics and Astronautics, 2005, 31(03): 265-269. (in Chinese)
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Trajectory control logic of space exploration rocket required to arrive given site with zero speed at given time

  • School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

  • Received Date: 29 Aug 2003
  • Publish Date: 31 Mar 2005
    Abstract
  • The special space exploration rocket is launched to rendezvous with the celestial body flying around earth, the absolute velocity of rocket should be zero at rendezvous time in order to satisfy the observe requirement. The ideal rendezvous orbit was designed before launch based on the orbit of the celestial body and launch site. The orbit parameters were loaded to onboard computer of rocket. After launch, the inertial navigation system was used to measure the rocket position and velocity, the thruster fire direction was adjusted try to eliminate the flight orbit errors. The several coordinated was defined and rocket orbit dynamical equation was created. The ideal rendezvous time, launch time and rendezvous point in space were studied. The trajectory control logic given during the thruster force is available. The error signal is decomposed into time error, altitude error, north-south error and east-west error in local horizontal frame. Position and velocity shift can be set to reduce the orbit drift caused by perturbation. The feasibility of control logic is verified by computer numerical simulation.

     

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  • [1] 肖业伦. 航天器飞行动力学原理[M] 北京:宇航出版社,1995 Xiao Yelun. Concept of space craft flight dynamics[M] Beijing:China Astronautics Press, 1995(in Chinese) [2] Frank A Marcos. Recent advances in satellite drag modeling . AIAA 99-0631, 1999 [3] 徐延万. 控制系统[M] 北京:宇航出版社,1989 Xu Yanwan. Control system[M] Beijing:China Astronautics Press, 1989(in Chinese) [4] 张守信. 外弹道测量与卫星轨道测量基础[M] 北京:国防工业出版社,1992 Zhang Shouxin. Trajectory tracking and satellite orbit measurement[M] Beijing:National Defense Industry Press, 1992(in Chinese) [5] 刘利生. 外测数据事后外理[M] 北京:国防工业出版社,2000 Liu Lishen. Post-flight data processing of trajectory measurement[M] Beijing:National Defense Industry Press, 2000(in Chinese)
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