Design of Flight Control System Based on Adaptive Backstepping Method for Space Transportation System

Author:

ABE Akio,IWAMOTO Kohei,SHIMADA Yuzo

Publisher

Japan Society for Aeronautical and Space Sciences

Reference26 articles.

1. 1) Menon, P. K. A., Badgett, M. E. and Walker, R. A.: Nonlinear Flight Test Trajectory Controllers for Aircraft, J. Guid., 10 (1987), pp. 67-72.

2. 2) Lane, S. H. and Stengel, R. F.: Flight Control Design Using Non-Linear Inverse Dynamics, Automatica, 24 (1988), pp. 471-483.

3. 4) Costa, R. R., Chu, Q. P. and Mulder, J. A.: Reentry Flight Controller Design Using Nonlinear Dynamic Inversion, J. Spacecraft Rockets, 40 (2003), pp. 64-71.

4. 5) Tanaka, N., Suzuki, S., Masui, K. and Tomita, H.: Restructurable Guidance and Control for Aircraft with Failures Considering Gust Effects, J. Guid. Control Dynam., 29 (2006), pp. 671-679.

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