A Tracking Differentiator Based Backstepping Control of Missile System
Authors
Wenguang Zhang, Lili Yang, Junwei Lei
Corresponding Author
Wenguang Zhang
Available Online January 2018.
- DOI
- 10.2991/macmc-17.2018.132How to use a DOI?
- Keywords
- Tracking differentiator; stability; Backstepping; Missile; Control system
- Abstract
To avoid the complex calculation of derivative in the backstepping design procedure, a novel kind of tracking differentiator was adopt to solve the derivative of ideal angle speed of the pitch channel missile system. Also, the ideal angle speed should be bounded or the stability of the system can not be guaranteed. And a Lyapunov function was chosen to prove the stability of the whole system. At last, the detailed numerical simulation was done to show the rightness and effectiveness of the proposed method.
- Copyright
- © 2018, 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 - Wenguang Zhang AU - Lili Yang AU - Junwei Lei PY - 2018/01 DA - 2018/01 TI - A Tracking Differentiator Based Backstepping Control of Missile System BT - Proceedings of the 2017 4th International Conference on Machinery, Materials and Computer (MACMC 2017) PB - Atlantis Press SP - 700 EP - 703 SN - 2352-5401 UR - https://doi.org/10.2991/macmc-17.2018.132 DO - 10.2991/macmc-17.2018.132 ID - Zhang2018/01 ER -