首页> 外文会议>AIAA infotech@aerospace conference >Predictor-Model-Based Least-Squares Model-Reference Adaptive Control with Chebyshev Orthogonal Polynomial Approximation
【24h】

Predictor-Model-Based Least-Squares Model-Reference Adaptive Control with Chebyshev Orthogonal Polynomial Approximation

机译:Chebyshev正交多项式逼近的基于预测模型的最小二乘模型参考自适应控制

获取原文

摘要

This paper presents a model-reference adaptive control approach for systems with unstructured uncertainty based on two least-squares parameter estimation methods: gradient-based method and recursive least-squares method. The unstructured uncertainty is approximated by Chebyshev orthogonal polynomial basis functions. The use of orthogonal basis functions improves the function approximation significantly and enables better convergence of parameter estimates. The adaptation of least-squares adaptive control is driven by the plant modeling error which manifests itself as the tracking error, but not vice versa. A predictor model is introduced to estimate the plant modeling error without the need for differentiation of the state signals which can introduce noise. The least-squares gradient adaptive control achieves superior parameter convergence as compared to the standard model-reference adaptive control. Flight control simulations were conducted with four adaptive controllers: least-squares gradient adaptive control, recursive least-squares adaptive control, standard model-reference adaptive control, and neural-network adaptive control. The results show that the recursive least-squares adaptive control achieves better robustness as measured by a time-delay margin while the least-squares gradient adaptive control achieves better tracking performance than both the standard model-reference adaptive control and neural-network adaptive control.
机译:本文介绍了基于两个最小二乘参数估计方法的具有非结构化不确定性的系统的模型参考自适应控制方法:基于梯度的方法和递归最小二乘法。非结构化的不确定性由Chebyshev正交多项式基本函数近似。正交基函数的使用显着提高了函数近似,并且能够更好地收敛参数估计。最小二乘自适应控制的适应由工厂建模误差驱动,这表明自己作为跟踪误差,但不反之亦然。引入预测测量模型以估计工厂建模误差,而无需对可以引入噪声的状态信号的差异化。与标准型号参考自适应控制相比,最小二乘梯度自适应控制实现了优异的参数收敛。使用四个自适应控制器进行飞行控制模拟:最小二乘梯度自适应控制,递归最小二乘自适应控制,标准模型参考自适应控制和神经网络自适应控制。结果表明,递归最小二乘自适应控制实现了通过时滞距离测量的更好的鲁棒性,而最小二乘梯度自适应控制实现比标准模型参考自适应控制和神经网络自适应控制更好地跟踪性能。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号