Adaptive integral dynamic surface control of a hypersonic flight vehicle

作者：Butt Waseem Aslam^*; Yan Lin; Amezquita Kendrick S

来源：International Journal of Systems Science, 2015, 46(10): 1717-1728.

DOI：10.1080/00207721.2013.828798

• dynamic surface control
• non-linear systems
• neural networks
• aircraft
• adaptive control

In this article, non-linear adaptive dynamic surface air speed and flight path angle control designs are presented for the longitudinal dynamics of a flexible hypersonic flight vehicle. The tracking performance of the control design is enhanced by introducing a novel integral term that caters to avoiding a large initial control signal. To ensure feasibility, the design scheme incorporates magnitude and rate constraints on the actuator commands. The uncertain non-linear functions are approximated by an efficient use of the neural networks to reduce the computational load. A detailed stability analysis shows that all closed-loop signals are uniformly ultimately bounded and the
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tracking performance is guaranteed. The robustness of the design scheme is verified through numerical simulations of the flexible flight vehicle model.

• 出版日期2015-7-27
• 单位北京大学