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对于拍翅式微型飞行器,设计了一种能产生大升力的翅拍动形式,分析计算了翅拍动所产生的气动力和气动力矩,导出了拍翅式微型飞行器机体的运动微分方程。利用该运动微分方程,可以对拍翅式微型飞行器的位置和姿态进行控制。
For the flapping-type micro-aircraft, a flapping-out form that can generate large lift force is designed. The aerodynamic force and aerodynamic moment generated by the flapping motion are analyzed and calculated, and the differential equations of motion of the flapping-type micro-aircraft body are derived. Using this differential equation of motion, the position and attitude of the flapping-type micro-aircraft can be controlled.