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基于径向基神经网络的空天飞行器鲁棒自适应轨迹线性化控制 被引量：2

Design of robust adaptive trajectory linearization controller for aerospace vehicles based on RBFNN
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摘要 基于轨迹线性化控制方法(TLC)以及径向基神经网络(RBFNN)技术研究了一种新的鲁棒自适应轨迹线性化控制方案并应用于空天飞行器(ASV)飞行控制系统设计中.首先基于被控对象的分析模型设计系统的TLC控制器,然后利用RBFNN对系统不确定的逼近能力,设计了鲁棒自适应控制器及参数的自适应调节律,并采用Lyapunov方法严格证明了闭环系统所有误差信号一致最终有界.最后应用新控制方案设计了ASV飞行控制系统,仿真结果表明了方法的有效性. This paper presents a novel robust adaptive trajectory linearization control （TLC） method based on radial basic function neural network （RBFNN） and introduces its application to an aero-space vehicle （ASV） flight control system. Firstly, the TLC controller was designed based on an analytical model of the control plant. Secondly, RBFNN was utilized to approximate the system＇s uncertainties, and based on which, a robust adaptive controller as well as an adaptive law were designed. Then, Lyapunov＇s direct method was used, and a rigorous poof was demonstrated in order to guarantee the ultimate boundedness of all the signals in the closed loop system of the provided method. Finally, the proposed method was applied to the flight control system design of ASV, and its effectiveness was verified by simulation results.
作者 薛雅丽 姜长生 朱亮
机构地区 南京航空航天大学自动化学院
出处 《航空动力学报》 EI CAS CSCD 北大核心 2008年第4期765-770,共6页 Journal of Aerospace Power
基金 国家自然科学基金(90405011)资助项目
关键词 轨迹线性化控制(TLC) 径向基神经网络(RBFNN) 鲁棒自适应控制 空天飞行器(ASV) trajectory linearization control （TLC） radial basic function neural network （RBFNN） robust adaptive control aerospace vehicles （ASV）
分类号 TP273.2 [自动化与计算机技术—检测技术与自动化装置]
  • 相关文献

参考文献8

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二级参考文献9

  • 1Mickle MC and Zhu J.Bank-to-turn roll-yaw-pitch autopilot design using dynamic nonlinear inversion and PD-eigenvalue assignment[A].In:Proceedings of the American Control Conference[C].Chicago:IEEE,2000:1359-1364
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共引文献25

同被引文献23

  • 1丁刚,徐敏强,侯立国.基于过程神经网络的航空发动机排气温度预测[J].航空动力学报,2009,24(5):1035-1039. 被引量：23
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  • 8Mickle M C,Zhu J. Bank-to turn roll-yaw-pitch autopilot design using dynamic nonlinear inversion and PD-eigenvalue assignment[ C]//Proceedings of the American Control Conference. Chicago: IEEE,2000:1359-1364.
  • 9Bevacqua T, Best E, Huizenga A, et al. Improved trajectory linearization flight controller for reusable launch vehicles [ C]//42nd AIAA Aerospace Sciences Meeting and Exhibit. Reno: AIAA,201M :1-16.
  • 10曾宪法,张磊,申功璋.基于动态逆和分散控制的导弹控制系统设计[J].北京航空航天大学学报,2007,33(11):1303-1307. 被引量：11

引证文献2

二级引证文献4

航空动力学报
2008年 第4期

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