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结合某轻型无人直升机的研制工作,以Simulink仿真平台建立了直升机飞行动力学模型,包含旋翼、机身、尾桨和运动方程等基本模块,对所受的力和力矩进行配平计算,得到平衡态的操纵量与机体姿态角,为操纵系统的电传化改装提供操纵量的参考值。
Combined with the development of a light unmanned helicopter, a helicopter flight dynamics model was established with Simulink simulation platform, including the basic modules of rotor, fuselage, tail rotor and motion equations, and balance the force and torque State manipulation and body attitude angle, for the manipulation of electrical conversion system to provide manipulation of the reference value.