作者: Penghui Fan , Chenxi Zhang , Xinhua Wang , Kaiyuan Cai
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摘要: The considered aircraft can provide an economical combination of vertical takeoff and landing (VTOL) capability with efficient high-speed cruise flight. sliding mode control laws are proposed in this paper for flight path tracking attitude to achieve the transition. Besides, a allocation algorithm based on law is designed. design overcomes defect original mode-transition which sensitive noise. By using design, under measurement noise reasonable. efficiency verified by simulations.