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- W2382757796 abstract "The design of aircraft landing control law is more complex than the design of common airplan mode control law.Pseudo-Inverse Method is used to reconfigure the control law when the left elevator is deadlocking in the process of flying-wing UAV automatic Landing,without changing the designed control law for normal airplane,moreover,its structure is simple.Because of the exclusive pneumatic layout and structure peculiarity of flying-wing UAV,the coupling character of the longitudinal and lateral control was considered in non-linear modeling of UAV.At the same time,Matlab/Simulink was used to complete the linear and non-linear simulation.The simulation results demonstrate that UAV can still perform landing safely and the method is simple and effective." @default.
- W2382757796 created "2016-06-24" @default.
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- W2382757796 date "2012-01-01" @default.
- W2382757796 modified "2023-09-27" @default.
- W2382757796 title "Application of Pseudo-Inverse Method in Control of UAV′s Safety Landing" @default.
- W2382757796 hasPublicationYear "2012" @default.
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