The Kinematics and Control of Relative Attitude Pointing for Spacecraft Formation Flying

摘要：

A geometric method which exploits the coupled relationship between relative position and relative attitude pointing is proposed to derive the desired relative attitude pointing Euler angles. The coupled kinematics and the dynamics equations of the relative attitude pointing are obtained. A sliding mode control based on exponent reaching law is applied to the coupled control system. The simulation results show the effectiveness of the coupled control system on the relative attitude pointing and relative position of spacecraft formation flying.

关键词： Spacecraft Formation Flying Coupled Control Attitude pointing Kinematics and Dynamics Sliding Mode Control

作者: YouTao Gao Bo Xu YuPing Lu

作者单位: College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, 2100 College of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, 2100

会议类型: 国际会议

会议名称: 2009年中国控制与决策会议(2009 Chinese Control and Decision Conference)

会议地点: 广西桂林

会议语种:英文

页码: 280-285

在线出版日期: 2009-06-17（万方平台首次上网日期，不代表论文的发表时间）