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大机动飞行的鲁棒自适应控制

The Robust Adaptive Control for High Maneuvers Flight
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摘要 针对飞机大机动飞行时存在的模型气动参数不确定性和外界扰动等影响因素,提出了一种基于反步法的鲁棒自适应滑模控制方法。基于反步的思想,适当选取李亚谱诺夫函数回馈递推得到不确定参数自适应律,并在最后一步结合线性滑模设计滑模控制器。对某飞机六自由度模型的大机动仿真验证了该方法的有效性。 A robust adaptive sliding mode controller based on backstepping is proposed for high maneuvers flight regarding model parameters uncertainties and unknown disturbance.The uncertain parameters adaptive law is obtained recursively via an appropriate choice of Lyapunov function based on backstepping procedure,and sliding mode controller is designed with the linear sliding mode in the last step.The high maneuvers flight simulation results for non-linear 6-DOF aircraft model show the effectiveness of the control method.
作者 周志久 刘波 孙勇
机构地区 北京航天自动控制研究所
出处 《航天控制》 CSCD 北大核心 2014年第1期35-39,共5页 Aerospace Control
关键词 大机动飞行 反步自适应 滑模控制 High maneuvers flight Backstepping Sliding mode control
分类号 TP273 [自动化与计算机技术—检测技术与自动化装置] V249.1 [航空宇航科学与技术—飞行器设计]
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参考文献7

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二级参考文献10

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共引文献6

航天控制
2014年 第1期

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