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基于无源性的带液体晃动月球着陆器的姿态控制 被引量：6

Passivity Based Attitude Control for Lunar Lander with Fuel Sloshing
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摘要 针对带液体晃动的月球着陆器提出了一种基于无源性的姿态控制方法.分析了由拉格朗日力学建立数学模型的带液体晃动的月球着陆器系统的特性,并证明了该系统的无源性.无源性保证了系统的输入输出稳定性,提出的Lyapunov函数保证了系统的内部稳定性.根据系统的无源性和提出的Lya-punov函数推导出基于无源性的控制方法.仿真结果表明,该方法能很好地达到控制效果. A passivity based attitude control method is proposed for lunar lander with fuel sloshing.The properties of lunar lander with fuel sloshing system modeled by Lagrange mechanics are analyzed,and its passivity is proved.The passivity guarantees the input-output stability and the proposed Lyapunov function guarantees the inner system stability.The control method is derived based on the passivity and the Lyapunov function.Simulation results are given to illustrate the validity.
作者 杜辉
机构地区 北京控制工程研究所 空间智能控制技术重点实验室
出处 《空间控制技术与应用》 2011年第1期50-54,共5页 Aerospace Control and Application
关键词 无源性 姿态控制 液体晃动 月球着陆器 passivity attitude control fuel sloshing lunar lander
分类号 V448 [航空宇航科学与技术—飞行器设计]
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参考文献8

  • 1Shageer H, Tao G. Modeling and adaptive control of spacecraft with fuel slosh: overview and case studies [ C ]. AIAA Guidance, Navigation, and Control Conference, Hiton Head, South Carolina, August 20-23, 2007.
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同被引文献47

  • 1周祥龙,赵景波.欠驱动非线性控制方法综述[J].工业仪表与自动化装置,2004(5):10-13. 被引量：13
  • 2王伟,易建强,赵冬斌,刘殿通.Pendubot的一种分层滑模控制方法[J].控制理论与应用,2005,22(3):417-422. 被引量：20
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  • 5Cho S, McClamroch N H, Reyhanoglu M. Feedback Control of a Space Vehicle with Unactuated Fuel Slosh Dynamics[ C]. A1AA Guidance, Navigation, and Con- trol Conference and Exhibit, Denver, CO, August 14- 17, 2000.
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  • 9于丹,岳宝增.一类带液体晃动欠驱动航天器的反馈控制[C].中国力学大会2011暨钱学森诞辰100周年纪念大会.哈尔滨:中国力学学会,2011.
  • 10Hassan K K. Adaptive Output Feedback Control of Non- linear Systems Represented by Input-Output Models [ J ]. IEEE Transactions on Automatic Control ( S0018- 9286), 1996, 41(2): 177-188.

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空间控制技术与应用
2011年 第1期

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