文章详细信息 关键词： 欠驱动航天器;;姿态稳定性;;滑模函数;;四元数 [gap=730]Keywords: underactuated spacecraft;attitude stabilization;sliding mode function;quaternion
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An integral type sliding mode function is adopted, the ideal control law is obtained from sliding mode theory.
采用一种积分型滑模函数，通过滑模理论推导出理想控制律。
参考来源 - 基于滑模理论的位置系统控制及摩擦力补偿·2,447,543篇论文数据，部分数据来源于NoteExpress
在设计控制系统时，滑模控制滑模面通过最小化最优价值函数得到，控制器采用饱和控制器。
In the process of control design, the sliding surface of sliding mode control is determined by minimizing the optimal cost function, and the controller is the saturation controller.
针对控制增益为未知常数和未知函数两种情形，分别提出分散自适应滑模控制器设计新方案。
Considering two cases that the system has constant control gains or function control gams, two novel decentralized adaptive sliding mode control schemes are presented, respectively.
在积分滑模控制与非线性微分控制中，分别给出了切换函数、非线性微分系数及控制器的设计方法。
Present the design method of switching function in integral sliding mode control, nonlinear derivative coefficient and controllers of DI-SVSC respectively.
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