A Continuous Multivariable Finite-Time Super-Twisting Attitude and Rate Controller for Improved Rotorcraft Handling

Aerospace

卷:9

Manfred Hajek¹  Omkar Halbe¹ 

[1] Institute of Helicopter Technology, Department of Aerospace and Geodesy, Technical University of Munich, Boltzmannstr. 15, 85748 Garching, Germany;

关键词: flight control;    robust control;    handling qualities;    sliding-mode control;   

DOI  :  10.3390/aerospace9010006

来源: DOAJ

【 摘 要 】

This paper synthesizes a continuous, multivariable, finite-time-convergent, super-twisting attitude and rate controller for rotorcraft with the objective of providing desired handling qualities and robustness characteristics. A sliding manifold is defined in the system state space to represent ideal attitude and rate command response dynamics of relative degree one with respect to the command input. Subsequently, robust command tracking is achieved via the synthesis of a multivariable super-twisting flight controller, which renders the plant states convergent on to the defined sliding manifold in finite-time and in the presence of matched external disturbance input. To validate the efficacy of the controller, simulation results are presented based on a nonlinear, higher-order rotorcraft model operating in turbulence. True system convergence to the sliding manifold from an untrimmed state is shown to lie within the theoretically predicted finite-time convergence bound. Furthermore, simulations with a linear quadratic flight controller are also presented for performance comparison with the proposed super-twisting flight controller.

【 授权许可】

Unknown