期刊文献+

小型无人直升机悬停状态下的系统辨识 被引量:2

System Identification on Small-scale Unmanned Helicopter
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摘要 提出了一种渐消记忆的最小二乘逐状态辨识算法,相对原来利用最小二乘进行无人直升机矩阵辨识的方法,该算法能极大地减小计算量,降低计算的复杂程度以提高计算过程的稳定性。并采用该方法建立了小型无人直升机系统的ARMAX模型和M IMO模型,还通过仿真对2种模型做了对比,结果显示M IMO模型能更精确地描述小型无人直升机系统。 This paper presents a fading memory based least squares identification method. Compared with the traditional system identification method applied on small scale unmanned helicopter, this method can reduce processing load and improve processing stability during identification. ARMAX model and MIMO model of small scale unmanned helicopter are sonstructed in this way and then do simulation on the models. The result shows that model of MIMO is more precise on representing the helicopter system.
出处 《重庆大学学报(自然科学版)》 EI CAS CSCD 北大核心 2007年第6期72-76,共5页 Journal of Chongqing University
基金 重庆市自然科学基金资助项目(2005BB2195)
关键词 无人直升机 MIMO ARMAX 系统辨识 最小二乘法 unmanned helicopter MIMO ARMAX system identification least squares
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参考文献8

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同被引文献17

  • 1吴红杰,袁世斐,谢旺.基于分数阶理论的锂离子电池动态模型及其参数辨识方法[J].新型工业化,2013,2(9):106-112. 被引量:3
  • 2陈仁良,谷伟岩,席华彬,于雪梅,张学军.直升机垂直飞行状态气动参数辨识方法研究[J].空气动力学学报,2006,24(1):115-119. 被引量:5
  • 3齐晓慧,田庆民,董海瑞.基于Matlab系统辨识工具箱的系统建模[J].兵工自动化,2006,25(10):88-90. 被引量:31
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