Landing Control System Design for a Flying-Wing Aircraft Based on ADRC

Author:

Wang Yanxiong,Zhu Xiaoping,Zhou Zhou,Shao Zhuang

Publisher

Springer International Publishing

Reference10 articles.

1. Snell, S.A., Nns, D.F., Arrard, W.L.: Nonlinear Inversion Flight Control for a Supermaneuverable Aircraft. AIAA Journal of Guidance, Control, and Dynamics 15(4), 976–984 (1992)

2. Sonneveldt, L., Chu, Q.P., Mulder, J.A.: Nonlinear Flight Control Design Using Constrained Adaptive Backsteepping. AIAA Journal of Guidance, Control, and Dynamics 30(2), 322–336 (2007)

3. Zhu, T.F., Li, M., Deng, J.H.: Nonlinear Flight Control System Based on Backstepping Theory and Supermaneuver. Acta Aeronautica Et Astronautica Sinica 26(4), 430–433 (2005)

4. Han, J.Q.: Active Disturbance Rejection Control Technique. National Defense Industry Press, Beijing (2009)

5. Xiao, Y.L., Jin, C.J.: Flight Theory of Atmospheric Disturbance. National Defense Industry Press, Beijing (1993)

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