Robust control for hypersonic vehicles with parametric and unstructured uncertainties

被引：5
|
作者：
Liu, Hao [1 ]
Liu, Deyuan [1 ]
Xi, Jianxiang [2 ]
Yu, Yao [3 ]
机构：
[1] Beihang Univ, Sch Astronaut, Beijing, Peoples R China
[2] High Tech Inst Xian, Xian 710025, Shaanxi, Peoples R China
[3] Univ Sci & Technol Beijing, Sch Automat & Elect Engn, Beijing, Peoples R China
来源：
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART C-JOURNAL OF MECHANICAL ENGINEERING SCIENCE | 2018年 / 232卷 / 13期
基金：
中国国家自然科学基金;
关键词：
Hypersonic vehicle; uncertain system; robust control; SLIDING MODE CONTROL; TRACKING-CONTROL; NONLINEAR CONTROL; ADAPTIVE-CONTROL; FLIGHT VEHICLE; AIRCRAFT; DESIGN;
D O I：
10.1177/0954406217720821
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
A robust flight controller is proposed for the longitudinal model of generic hypersonic vehicles, whose dynamics involves nonlinearities, parameter uncertainties, and unstructured uncertainties. The proposed longitudinal controller is developed based on the standard H theory and the robust compensating approach. The robust compensating approach is introduced to reduce the influences of multiple uncertainties and nonlinearities on the closed-loop control system. Compared to the H control theory, these influences in the whole frequency range can be restrained. Theoretical analysis and numerical simulation results are presented to illustrate the tracking performance properties of the designed robust control approach.
引用
收藏
页码：2369 / 2380
页数：12
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