Integrated Guidance and Control Based on Backstepping and Input-to-State Stability
This paper presents an approach of integrated guidance and control (IGC) design for interception of maneuvering targets (evaders). An IGC model with uncertainties in the pitch plane is formulated,and the IGC approach is developed via backstepping scheme. Theoretical analysis is shown that the design approach makes the line-of-sight (LOS) rate be input-to-state stable (ISS) with respect to target maneuvers and missile model uncertainties,and the stability of the missile dynamics can be guaranteed as well. The numerical simulation con.rms the effectiveness of the proposed design approach.
YAN Han JI Haibo
Department of Automation,University of Science and Technology of China,Hefei 230026,P.R.China
国际会议
The 30th Chinese Control Conference(第三十届中国控制会议)
烟台
英文
1-5
2011-07-01（万方平台首次上网日期，不代表论文的发表时间）