Induced L2 Norm Control for Missile Early-warning Satellite Attitude Maneuver

摘要：

In this paper, the Missile Early Warning Satellite Attitude Control problem is introduced, A two step incorporated and systematic method for modeling and control of missile early warning satellite is formulated. Firstly, the nonlinear dynamic and kinematics equation of the missile early warning satellite are reformulated to linear parameter variation (LPV) system. Secondly, based on the LPV model, an induced 2 L norm controller is introduced to eliminate the affect caused by the rotation of onboard mobile facilities, the designed LPV controller can guarantee that the induced 2 L norm from disturbance to attitude tracking error is less than a pre-given number. The LPV controller design problem is solved by Sum of Squares (SOS) programming techniques. The effectiveness of the proposed control technique is shown in simulations

关键词： missile early-warning satellite:attitude control mobile facilities:linear parameter variation(LPV):induced L2 norm control

作者: Zeng Ming Wang Jia Yu Zhiwei Ma Guangfu Wu Zhipeng

会议类型: 国际会议

会议名称: The 3rd International Symposium on Systems and Control in Aeronautics and Astronautics(第三届航空航天系统与控制国际会议 ISSCAA 2010)

会议地点: 哈尔滨

会议语种:英文

页码: 587-592

在线出版日期: 2010-01-08（万方平台首次上网日期，不代表论文的发表时间）