Author:
Zhong Sheng,Huang Yi,Chen Sen,Dai Lin
Publisher
Springer Science and Business Media LLC
Subject
Control and Optimization,Aerospace Engineering,Control and Systems Engineering
Reference20 articles.
1. Pan, C., Rong, J., Xu, T., & Xiang, D. (2020). Novel approach for active vibration control of a flexible missile. Defence Technology, 16(4), 956–967.
2. Su, C., Wang, X., Xu, Z., Li, J., & Wang, X. (2019). Research on elastic vibration suppression of missile attitude control system. Journal of Projectiles, Rockets, Missiles and Guidance, 39(5), 154–157 (in Chinese).
3. Oh, C., Bang, H., & Park, C. (2008). Attitude control of a flexible launch vehicle using an adaptive notch filter: ground experiment. Control Engineering Practice, 16(1), 30–42.
4. Wang, Z., & Liu, Z. (2010). Aero-elastic stability design of spinning ballistic missile with sliding mode control. In International Conference on Computer Design and Applications (pp. 3147–3152). Qinhuangdao, China.
5. Khoshnood, A. M., Roshanian, J., & Jafari, A. A. (2010). An adjustable model reference adaptive control for a flexible launch vehicle. Journal of Dynamic Systems, Measurement, and Control, 132(4), 1–7.
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