Adaptive sliding mode control for missile guidance law
- Resource Type
- Conference
- Authors
- Wu, Xiangyang; Bi, Shihua; Zhu, Zheng; Wu, Weinan
- Source
- Proceedings of the 33rd Chinese Control Conference Control Conference (CCC), 2014 33rd Chinese. :960-965 Jul, 2014
- Subject
- Computing and Processing
Robotics and Control Systems
Signal Processing and Analysis
Transportation
Acceleration
Missiles
Trajectory
Estimation
Closed loop systems
Sliding mode control
Adaptive systems
Guidance law
Adaptive control
- Language
- ISSN
- 1934-1768
The problem of missile interception is investigated in this paper. Sliding mode controllers are proposed for the design of guidance laws. Specially, the control design consists of the estimation of the target acceleration by adaptive scheme and thus it achieves the decrease of undesired chattering effectively. Also, simulation results are presented to illustrate the effectiveness of the control strategies.