| Citation: | LI Jiguang, CHEN Xin, LI Yajuan, et al. Nonlinear robust control method for maneuver flight of flying wing UAV[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(1): 89-98. doi: 10.13700/j.bh.1001-5965.2017.0014(in Chinese)
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As flying wing UAV lacks manipulating ability, a control strategy combined with fluidic thrust vectoring-turbocharged engine (FTV-E) technology is proposed. In this paper, the control scheme is designed:the inner loop compensator is used to eliminate the negative coupling term of system; the outer loop compensator used backstepping tracking algorithm; the particle swarm optimization (PSO) compensator to compensate the disturbance and coupling term that cannot be modeled. The control structure's stability is proved. Based on the traditional backstepping control methods, the proposed controller increases the inner loop compensator. The proposed inner loop compensator retains the aerodynamic damping term which is favorable to flight. This compensator not only can reduce the conservatism of the outer loop controller, but also is convenient for engineering realization. The simulation results show that the proposed control scheme is effective.
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