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- W2367721004 abstract "The airborne dispenser has high inter-channel coupling and serious parameter variation in dynamics.The autopilot for Bank-To-Turn(BTT) missiles designed according to conventional method usually uses independent design for each channel,and decreases the coupling and sideslip angle by compensation control,which has poor anti-interference capability. Robust problems in such designed flight control systems are severe.We studied the autopilot design approach to airborne dispenser in middle guidance phase by considering 3-channel as independent based on H∞ control theory.The inter-channel coupling effects between roll,yaw,and pitch channels are considered,but taken as bounded uncertainties.The controllers for each control channel are designed using suboptimal H∞ feedback.Six-DOF simulations are performed with square-wave pitch command,sine-wave roll command and zero yaw command.The results show that the controllers have high performance for set-point tracking in roll and pitch channels,with negligible side-slip angle in yaw channel,significantly improve the robustness to coupling factors and uncertainties in system parameters as compared with the traditional approach." @default.
- W2367721004 created "2016-06-24" @default.
- W2367721004 creator A5026817851 @default.
- W2367721004 date "2008-01-01" @default.
- W2367721004 modified "2023-09-23" @default.
- W2367721004 title "Autopilot design and digital simulation for airborne dispenser based on H_∞ robustness control" @default.
- W2367721004 hasPublicationYear "2008" @default.
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