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The motion decomposition of power descent section of soft landing on small bodies based on sliding mode and PD control algorithm

机译:基于滑模和PD控制算法的小飞机软着陆下降段运动分解

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In view of the power descent section of soft landing on small bodies, this paper had deduced the system dynamic models of the probe near small bodies under the body-fixed coordinate system. Through the analysis of the model, we decomposed this one phase of the movement into the out-of-plane movement and in plane movement based on the orbital plane. To the out-of-plane movement, a nominal height trajectory had been projected and variable structure control (VSC) with sliding mode had been designed to track the nominal trajectory. To the in plane movement, according to the coupling of movement and the desired final state, PD controllers are designed to eliminate the deviation of position and velocity. Finally, the effectiveness of algorithms were verified by numerical simulation.
机译:鉴于小物体软着陆的功率下降部分,本文推导了在小物体固定坐标系下小物体附近探头的系统动力学模型。通过对模型的分析,我们将运动的这一阶段分解为基于轨道平面的平面外运动和平面内运动。对于平面外运动,已投影了标称高度轨迹,并设计了带有滑模的可变结构控制(VSC)来跟踪标称轨迹。对于平面内运动,根据运动和所需的最终状态的耦合,设计了PD控制器以消除位置和速度的偏差。最后,通过数值仿真验证了算法的有效性。

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