Integrated Guidance and Control for a Missile in the Pitch Plane Based upon Subspace Stabilization
Based upon the model of the relative motion between the missile and the target and the model of the missile moving in the pitch plane, a novel integrated guidance and control model under the error tracking meaning is established. It is different from the state-equation-based integrated guidance and control models, it emphasizes particularly on attitude angles tracking. Especially, the realization of the error tracking properties is turned into the corresponding parameters adjusting by subspace stabilization technology. The globally asymptotical stabilization of the error tracking system is realized by an observer with the adaptive adjusting function about the model error and about the target maneuverability. The simulation results indicate that the design is effective.
missile integrated guidance and control subspace stabilization observer
Sang Baohua Jiang Changsheng
College of Aviation Technology, NUAA, Jiangsu, Nanjing. 210016, China Department of Automation Engineering, NUAA, Jiangsu, Nanjing. 210016, China
国际会议
2009年中国控制与决策会议(2009 Chinese Control and Decision Conference)
广西桂林
英文
5409-5414
2009-06-17（万方平台首次上网日期，不代表论文的发表时间）