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一种空间交会绕飞段的小推力滑移制导方法
引用本文:刘鲁华,郑伟,汤国建.一种空间交会绕飞段的小推力滑移制导方法[J].空间控制技术与应用,2010,36(1):46-50.
作者姓名:刘鲁华  郑伟  汤国建
作者单位:国防科技大学航天与材料工程学院,长沙,410073
摘    要:小推力技术在空间交会任务中应用前景巨大,可用于长期绕飞和快速绕飞任务.研究滑移制导方法在空间绕飞中的具体应用,给出任意空间绕飞任务的描述方式,推导任意平面内的圆轨道绕飞和椭圆轨道绕飞公式.考虑实际工程需要,研究基于小推力发动机的滑移制导方法在工程上的实现问题,仿真验证了小推力技术在绕飞任务中的工程可行性.

关 键 词:空间交会  小推力  绕飞  滑移制导

A Low-Thrust Glidescope Guidance in Fly-Around Phase of Space Rendezvous
LIU Luhua,ZHENG Wei,TANG Guojian.A Low-Thrust Glidescope Guidance in Fly-Around Phase of Space Rendezvous[J].Aerospace Contrd and Application,2010,36(1):46-50.
Authors:LIU Luhua  ZHENG Wei  TANG Guojian
Institution:College of Astronautical & Material Engineering/a>;National University of Defense Technology/a>;Changsha 410073/a>;China
Abstract:The low-thrust technique used in long duration or rapid fly-around phase has an enormous potential in space rendezvous mission. Based on the glidescope guidance approach the paper studies the space fly-around technique. A glidescope guidance in fly-around application is studied; the circle and ellipse fly-around equations are deduced. The implementation problem is analyzed and resolved based on the low-thrust technique. Simulation results validate feasibility of the low-thrust technique in fly-around missio...
Keywords:space rendezvous  low-thrust  fly-around  glidescope guidance  
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