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高超声速飞行器轨迹跟踪控制仿真研究 被引量：6

Simulation Research on Tracking Control for Hypersonic Aircraft
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摘要 针对高超声速飞行器纵向模型的快时变、强耦合和高度非线性的特点,在考虑模型不确定性的情况下,采用李导数的方法对某型高超声速飞行器进行输入输出的精确线性化。基于线性化后的模型,提出一种非线性动态逆控制的方法,并对其稳定性进行分析,实现对该型高超声速飞行器的轨迹跟踪控制。并利用Matlab搭建仿真平台,仿真结果显示仿真平台的正确性和控制算法的有效性。 Aiming at the significant feature that the hypersonic aircraft is fast time-varying,strong coupling and highly nonlinear,Lie derivative was adopted for Input-Output linearization to a hypersonic aircraft with uncertainties.Based on the linearized model,a dynamic inversion tracking controller was proposed,and stability analysis was given.Then a simulation platform was built based on Matlab.Simulation results show the correctness of the simulation platform and the effectiveness of the control approach.
作者 谭湘敏 易建强 赵冬斌 郝银星
机构地区 中国科学院自动化研究所复杂系统与智能科学重点实验室
出处 《系统仿真学报》 CAS CSCD 北大核心 2011年第4期745-749,共5页 Journal of System Simulation
基金 中科院知识创新工程重大项目子项目(ZKYGC08A02)
关键词 高超声速飞行器 线性化 动态逆 轨迹跟踪控制 hypersonic aircraft linearization dynamic inversion tracking control
分类号 TP391 [自动化与计算机技术—计算机应用技术]
  • 相关文献

参考文献7

  • 1Moses P L, Rausch V L, Nguyen L T, et al. NASA hypersonic flight demonstrators: overview, status, and future plans [J]. Acta Astronautica (S0094-5765), 2004, 55(3-9): 619-630.
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  • 3Xu H J, Ioannou P A, Mirmirani M. Adaptive sliding mode control design for hypersonic flight vehicle [J]. Journal of Guidance, Control and Dynamics (S0731-5090), 2004, 27(5): 829-838.
  • 4Huo Y, Mirmirani M, Ioannou P A, Kuipers M. Altitude and velocity tracking control for an airbreathing hypersonic cruise vehicle [C]// AIAA Guidance, Navigation, and Control Conference and Exhibit. Colorado, USA: AIAA, 2006: 1305-1315.
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二级参考文献12

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共引文献14

同被引文献67

引证文献6

二级引证文献27

系统仿真学报
2011年 第4期

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