论文部分内容阅读
针对仿鸟扑翼飞行器的柔性翼动力学仿真需要,在非定常空气动力学原理下,用修正的准定常气动力计算模型估算出了扑翼的动力学模型,并建立了其相应的状态空间方程,进而分析研究了在Matlab语言和Simulink环境下,对其仿真系统设计得需求和要求。
In order to simulate the flexible wing dynamics of the simulated flapping wing aircraft, the dynamic model of the flapping wing is estimated by the modified quasi-steady aerodynamic model under unsteady aerodynamics and its corresponding state space is established Then we analyze and study the requirements and requirements of the simulation system in Matlab language and Simulink environment.