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Research on the Lander Stability During Lunar Rover Unloading Base on the Theory of ZMP

机译:ZMP理论升降基地陆罗坡卸载过程中的登陆稳定性研究

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The function of the elevator is to help lunar rover arrive lunar surface from the top of Lander after landing. Rocker-arm elevator makes Lander overturn easily because its arm is too long. Different compress extent of the Lander leg, complicated condition of landing location, micro-gravity and unloading acceleration have great influence to the stability of Lander. The paper set the ZMP coordinate equation and the coordinate of support polygon by D-H coordinate law, and builds the rule of the stability. Example simulation result shows that the equation and the rule meet the requirement of Lander stability analysis on all different conditions.
机译:电梯的功能是帮助Lunar Rover从登陆后从着陆器顶部到达月球表面。 Rocker-Arm电梯使Lander轻松推翻,因为它的手臂太长。 着陆位置的不同压缩范围,着陆位置的复杂条件,微重力和卸载加速度对着陆器的稳定性有很大影响。 本文通过D-H协调法将ZMP坐标方程和支持多边形的坐标设置,并构建了稳定性的规则。 示例仿真结果表明,方程式和规则符合对所有不同条件的着陆稳定性分析的要求。

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