【摘 要】
：
基于欧拉角的变换得到了刚体飞行器的一种多模型自适应控制律,它能解决转动惯量不确定并随时发生突变的分导飞行器的姿态控制问题.该控制策略可以有效地检测出转动惯量发生突
【机 构】
：
哈尔滨工业大学控制理论与制导技术研究中心,
论文部分内容阅读
基于欧拉角的变换得到了刚体飞行器的一种多模型自适应控制律,它能解决转动惯量不确定并随时发生突变的分导飞行器的姿态控制问题.该控制策略可以有效地检测出转动惯量发生突变,并及时切换到最合适的控制器.通过理论分析证明了该控制策略的闭环全局渐近稳定.数值仿真表明该方案的有效性.
Based on the Euler angle transformation, a multi-model adaptive control law of rigid-body aircraft can be obtained, which can solve the attitude control problem of the fractional-guided aircraft whose moment of inertia is uncertain and change from time to time.The control strategy can effectively detect moment of inertia And the controller is switched to the most appropriate controller in time.The theoretical analysis shows the closed-loop global asymptotic stability of the control strategy.The numerical simulation shows the effectiveness of the proposed scheme.
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