Four-rotor aircraft control method based on improved MPC-PID

The invention provides a four-rotor aircraft control method based on improved MPC-PID. The method comprises the following steps: firstly, establishing a dynamic model of a four-rotor aircraft according to the four-rotor aircraft structure and mechanics principles, and transforming the dynamic model...

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Hauptverfasser: WANG SHENGSHUO, WU SHEN, ZHANG JIUJIANG, LIU HONGXIA, ZHANG DEHAI, FEI ZHIGEN, WANG CAIDONG, XIAO YANQIU, WANG HUI, WANG JIANHUI
Format: Patent
Sprache:chi ; eng
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