Adaptive BackStepping Sliding Mode Attitude Tracking of Rigid Spacecraft with di

rongq08731 23 0 PDF 2020-04-16 03:04:37

基于扰动的刚体飞行器自适应反推滑模控制，路坤锋，夏元清，这篇文章研究了刚体飞行器的姿态跟踪控制问题。利用滑模控制技术和反推技术,设计了一个新的自适应控制器,其不仅能完成精确的飞行�

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