DocumentCode
1362030
Title
Impact Time and Angle Guidance With Sliding Mode Control
Author
Harl, Nathan ; Balakrishnan, S.N.
Author_Institution
Department of Mechanical and Aerospace Engineering, Rolla,
Volume
20
Issue
6
fYear
2012
Firstpage
1436
Lastpage
1449
Abstract
A novel sliding mode-based impact time and angle guidance law for engaging a modern warfare ship is presented in this paper. In order to satisfy the impact time and angle constraints, a line-of-sight rate shaping process is introduced. This shaping process results in a tuning parameter that can be used to create a line-of-sight rate profile to satisfy the final time and heading angle requirements and to yield acceptable normal acceleration values. In order to track the desired line-of-sight rate profile in the presence of uncertainties, a novel robust second-order sliding mode control law is developed using a backstepping concept. Due to the robustness of the control law, it can be applied to many realistic engagement scenarios which include uncertainties such as target motion. Numerical simulations with different warship engagements are presented to illustrate the potential of the developed method.
Keywords
Marine vehicles; Missiles; Nonlinear control systems; Path planning; Sliding mode control; Uncertainty; Missiles; nonlinear control systems; path planning; sliding mode guidance;
fLanguage
English
Journal_Title
Control Systems Technology, IEEE Transactions on
Publisher
ieee
ISSN
1063-6536
Type
jour
DOI
10.1109/TCST.2011.2169795
Filename
6060928
Link To Document