Abstract
This paper is devoted to attitude control of a nonlinear missile model. Combining the back-stepping technique, the corresponding sliding mode controller is designed to guarantee the state variables of the closed loop system to converge to the reference state with the help of the adaptive law by estimating the total uncertainties. Also, simulation results are presented to illustrate the effectiveness of the control strategy.
Original language | English |
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Pages (from-to) | 1937-1944 |
Number of pages | 8 |
Journal | ICIC Express Letters |
Volume | 4 |
Issue number | 5 B |
Publication status | Published - Oct 2010 |
Keywords
- Adaptive control
- Back-stepping
- Missile attitude Control
- Sliding mode control
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Lin, Z., Zhu, Z., Xia, Y., & Wang, S. (2010). Adaptive control for missile systems with parameter uncertainty. ICIC Express Letters, 4(5 B), 1937-1944.