中国科学院机构知识库网格系统: Adaptive control at launching using three loop autopilot (EI CONFERENCE)

中国科学院机构知识库网格

Chinese Academy of Sciences Institutional Repositories Grid

Adaptive control at launching using three loop autopilot (EI CONFERENCE)

文献类型：会议论文


作者	Zhang Y.
出版日期	2011
会议名称	2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011, July 15, 2011 - July 17, 2011
会议地点	Inner Mongolia, China
关键词	In order to guarantee the precise initial flight trajectory control the missile disturbance of large disturbance torque three loop adaptive autopilot was researched. The characteristics of the projectile and three loop autopilot instruction formation characteristics were analysed. From equivalent pitching angle of lateral acceleration feedback loop combined with the instruction of generalized error autopilot structure was simplified and three loop autopilot adaptive control law and stability were designed. The test data show that when disturbance torque was 600Nm the attitude angle generalized error was -4.4. In the time lasted about 15s late trajectory accuracy was within 1.0.Three loop autopilot adaptive control law was able to control the disturbance of initial trajectory and adapt to dynamic characteristics changes control system stability. It was the initial trajectory accurate solution method of flight. 2011 IEEE.
页码	5535-5538
收录类别	EI
源URL	[http://ir.ciomp.ac.cn/handle/181722/33452]
专题	长春光学精密机械与物理研究所_中科院长春光机所知识产出_会议论文
推荐引用方式 GB/T 7714	Zhang Y.. Adaptive control at launching using three loop autopilot (EI CONFERENCE)[C]. 见:2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011, July 15, 2011 - July 17, 2011. Inner Mongolia, China.

入库方式： OAI收割

来源：长春光学精密机械与物理研究所

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