Active Disturbance Rejection Control for Attitude Control of Missile Systems Based on Back-stepping Method
Author:
Publisher
Springer Science and Business Media LLC
Subject
Computer Science Applications,Control and Systems Engineering
Link
https://link.springer.com/content/pdf/10.1007/s12555-019-0988-2.pdf
Reference28 articles.
1. Y. Xia, K. Lu, Z. Zhu, and M. Fu, “Adaptive back-stepping sliding mode attitude control of missile systems,” International Journal of Robust & Nonlinear Control, vol. 23, no. 15, pp. 1699–1717, 2013.
2. Y. Yao, B. Yang, F. He, Y. Qiao, and D. Cheng, “Attitude control of missile via fliess expansion,” IEEE Transactions on Control Systems Technology, vol. 16, no. 5, pp. 959–970, 2008.
3. W. Luo, Y. Chu, and K. Ling, “Inverse optimal adaptive control for attitude tracking of spacecraft,” IEEE Transactions on Automatic Control, vol. 50, no. 11, pp. 1639–1654, 2005.
4. M. Lovera and A. Astolfi, “Spacecraft attitude control using magnetic actuators,” Automatica, vol. 40, no. 8, pp. 1405–1414, 2004.
5. P. Crouch, “Spacecraft attitude control and stabilization: Applications of geometric control theory to rigid body models,” IEEE Transactions on Automatic Control, vol. 29, no. 4, pp. 321–331, 2003.
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