Adaptive Sliding Mode Control with Backstepping Approach for a Moving Mass Hypersonic Spinning Missile

DOI

10.2991/asei-15.2015.163How to use a DOI?

Keywords

adaptive sliding mode control; backstepping; spinning missile; moving mass.

Abstract

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.

Copyright

© 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/).

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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  -