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在空间布局紧凑条件下,通过对某无人机主起落架舱门收放空间的分析,实现了舱门和起落架的联动收放设计,并通过仿真验证对其收放状态进行描述。此方法可作为同类型无人机起落架与舱门联动设计的参考。
Under the condition of compact space layout, through the analysis of the retractable space of main landing gear door of a UAV, the design of interlocking retractable door and landing gear was realized, and its retractable status was described through simulation. This method can be used as a reference for the same type UAV landing gear and door interlocking design.