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针对由于襟翼操纵系统刚强度不足导致襟翼偏角角度不足,无人机滑行距离过长的问题,提出了无人机襟翼操纵系统的改进设计方法,详细介绍了某无人机襟翼操纵系统改进方案。在襟翼操纵系统有限元仿真分析和力学实验结果的基础上,解析当前襟翼操纵系统存在的关键问题,并针对该问题提出了相应的解决方案,对襟翼操纵系统的结构形式进行改进,更换了襟翼结构材料,提高了襟翼操纵系统可靠性,为襟翼操纵系统的结构设计提供了理论基础和可行性设计方法。
Aiming at the problem that the flight angle of the unmanned aircraft is too short due to the lack of the strength of the flap control system, the improved design method of the UAV flap control system is proposed. Control system improvement program. Based on the finite element simulation analysis and mechanical experiment results of the flap control system, the key problems existing in the flap control system are analyzed, and corresponding solutions are put forward to improve the structure of the flap control system. The flaps structure materials improve the reliability of the flap control system and provide the theoretical basis and feasibility design method for the structural design of the flap control system.