Adaptive Sliding Mode Control with Backstepping Approach for a Moving Mass Hypersonic Spinning Missile
- 10.2991/asei-15.2015.163How to use a DOI?
- adaptive sliding mode control; backstepping; spinning missile; moving mass.
The dynamics model of a hypersonic spinning missile with two moving masses is established. Considering the inherent uncertainties of the mathematical model and the aerodynamic parameters, an affine model with external disturbances is established and an attitude adaptive sliding mode controller is designed following the backstepping approach. The stability of the closed-loop system is proved by means of Lyapunov method. A saturation function is introduced to eliminate the chattering of the sliding mode controller, and the numerical simulations show that the attitude controller is effective.
- © 2015, the Authors. Published by Atlantis Press.
- Open Access
- This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).
Cite this article
TY - CONF AU - Feng-Jie Gao AU - Liang-Yu Zhao PY - 2015/05 DA - 2015/05 TI - Adaptive Sliding Mode Control with Backstepping Approach for a Moving Mass Hypersonic Spinning Missile BT - Proceedings of the 2015 International conference on Applied Science and Engineering Innovation PB - Atlantis Press SP - 834 EP - 837 SN - 2352-5401 UR - https://doi.org/10.2991/asei-15.2015.163 DO - 10.2991/asei-15.2015.163 ID - Gao2015/05 ER -