所属单位：自动化学院
发表刊物：ISA TRANSACTIONS
关键字：Flying-boom aerial refueling Sliding mode control Double power reaching law Active disturbance rejection control Relative position-keeping
摘要：This paper proposes the design of the relative position-keeping control of the receiver unmanned aerial vehicle (UAV) with the time-varying mass in the refueling phase utilizing an inner-outer loop structure. Firstly, the model of the receiver in the refueling phase is established. And then tank model is set up to analyze the influence of fuel transfer on the receiver. Subsequently, double power reaching law based sliding mode controller is designed to control receiver translational motion relative to tanker aircraft in the outer loop while active disturbance rejection control technique is applied to the inner loop to stabilize the receiver. In addition, the closed-loop stabilities of the subsystems are established, respectively. Finally, an aerial refueling model under various refueling strategies is utilized. Simulations and comparative analysis demonstrate the effectiveness and robustness of the proposed controllers. (C) 2017 ISA. Published by Elsevier Ltd. All rights reserved.
ISSN号：0019-0578
是否译文：否
发表时间：2018-02-01
合写作者：An, Shuai
通讯作者：袁锁中
发表时间：2018-02-01