倾转旋翼机平均驻留时间切换鲁棒H∞跟踪控制

针对倾转旋翼飞行器模态转换阶段的飞行控制问题,本文给出了倾转旋翼机纵向运动飞行控制系统模型和一种基于参考模型的鲁棒跟踪控制方法.为了保证闭环系统在切换过程中稳定并同时满足指定的鲁棒H∞性能指标,利用状态观测器对系统不可观测状态进行估计,结合模型依赖平均驻留时间方法提出了一种倾转旋翼机切换鲁棒H∞跟踪控制方法,通过求解线性矩阵不等式得到控制器增益,并分析了系统的鲁棒稳定性.仿真结果表明,所提出的方法能够使飞行器系统准确跟踪指令,且对于控制器切换具有鲁棒性....

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Published in控制理论与应用 Vol. 37; no. 5; pp. 1018 - 1027
Main Authors 杨洁, 陈谋, 熊师洵, 熊英
Format Journal Article
LanguageChinese
Published 南京航空航天大学自动化学院,江苏南京,210016 01.05.2020
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ISSN1000-8152
DOI10.7641/CTA.2019.90235

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Abstract 针对倾转旋翼飞行器模态转换阶段的飞行控制问题,本文给出了倾转旋翼机纵向运动飞行控制系统模型和一种基于参考模型的鲁棒跟踪控制方法.为了保证闭环系统在切换过程中稳定并同时满足指定的鲁棒H∞性能指标,利用状态观测器对系统不可观测状态进行估计,结合模型依赖平均驻留时间方法提出了一种倾转旋翼机切换鲁棒H∞跟踪控制方法,通过求解线性矩阵不等式得到控制器增益,并分析了系统的鲁棒稳定性.仿真结果表明,所提出的方法能够使飞行器系统准确跟踪指令,且对于控制器切换具有鲁棒性.
AbstractList 针对倾转旋翼飞行器模态转换阶段的飞行控制问题,本文给出了倾转旋翼机纵向运动飞行控制系统模型和一种基于参考模型的鲁棒跟踪控制方法.为了保证闭环系统在切换过程中稳定并同时满足指定的鲁棒H∞性能指标,利用状态观测器对系统不可观测状态进行估计,结合模型依赖平均驻留时间方法提出了一种倾转旋翼机切换鲁棒H∞跟踪控制方法,通过求解线性矩阵不等式得到控制器增益,并分析了系统的鲁棒稳定性.仿真结果表明,所提出的方法能够使飞行器系统准确跟踪指令,且对于控制器切换具有鲁棒性.
Author 陈谋
熊师洵
熊英
杨洁
AuthorAffiliation 南京航空航天大学自动化学院,江苏南京,210016
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XIONG Ying
CHEN Mou
XIONG Shi-xun
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Keywords 倾转旋翼飞行器
状态观测
平均驻留时间
鲁棒H∞控制
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Title 倾转旋翼机平均驻留时间切换鲁棒H∞跟踪控制
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