火力与指挥控制2012，Vol.37Issue(7)：91-94,4.
高超音速飞行器参数不确定性的自适应控制方法
An Adaptive Control Method for Uncertain Parameters of a Hypersonic Vehicle
王首斌 1王新民 1姚从潮 1黄誉1
作者信息
- 1. 西北工业大学自动化学院,西安710129
- 折叠
摘要
Abstract
In order to deal with uncertain parameters of a general hypersonic vehiclet longitudinal movement control law is designed based on the theory of simple adaptive control. How to establish a longitudinal movement model and a reference model and how to design adaptive control law with adaptive control theory are illustrated. Numerical simulation is done to validate robustness of the flight control law. Simulation results show that the control performance can satisfy with adaptively regulate control coefficients due to the errors of the outputs between the refernce model and the hypersonic vehicle. This method is effective and dealt with the problem of uncertain parameters preferably.关键词
高超音速飞行器/简单自适应控制/参数不确定性Key words
hypersonic vehicle/simple adaptive control/uncertain parameters分类
信息技术与安全科学引用本文复制引用
王首斌,王新民,姚从潮,黄誉..高超音速飞行器参数不确定性的自适应控制方法[J].火力与指挥控制,2012,37(7):91-94,4.
