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Feedback linearization based sliding mode control system for quad-rotor UAV with a Ground effect
Feedback linearization based sliding mode control system for quad-rotor UAV with a Ground effect
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机译:具有地面效应的四旋翼无人机基于反馈线性化的滑模控制系统
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摘要
The present invention relates to a sliding mode control system based on feedback linearization for a quadrotor having a ground effect, and the attitude of a quadrotor stable against disturbances such as ground effects by a sliding mode control designing a closed loop integral type as a sliding plane It is characterized in that it can have maintenance and position control performance.
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