Finite-time output tracking control for air-breathing hypersonic vehicles with actuator constraints

被引:32
作者
An, H. [1 ]
Xia, H. [1 ]
Wang, C. [1 ]
机构
[1] Harbin Inst Technol, Space Control & Inertial Technol Res Ctr, Xidazhi St 92, Harbin 150001, Peoples R China
基金
中国国家自然科学基金;
关键词
Air-breathing hypersonic vehicles (AHVs); finite-time tracking; input saturation; nonsingularity and free-chattering; feedback linearization; SLIDING-MODE CONTROL; ROBUST NONLINEAR CONTROL; FLIGHT VEHICLE; CONTROL DESIGN; DISCRETE-TIME; SYSTEMS; GUIDANCE; MAGNITUDE; STABILITY; AIRCRAFT;
D O I
10.1177/0954410016675894
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper designs a finite-time output tracking controller for air-breathing hypersonic vehicles (AHVs) subjected to disturbances and actuator constraints. After proper derivations, the original model is divided into two independent subsystems undergoing mismatched lumped disturbance. A finite-time disturbance observer (FTDO) is employed to estimate the lumped disturbance, while an auxiliary system combined with a command pre-filter is designed to analyze the effect of input saturation caused by the restrained actuators. Based on the FTDO and the auxiliary system, a novel integral sliding surface is constructed and then a chattering-free nonsingular controller is developed to realize finite-time output tracking in spite of mismatched lumped disturbance and input saturation, which is its major merit compared with other existing AHV controllers. A simulation study is carried out to verify the proposed control scheme.
引用
收藏
页码:2578 / 2593
页数:16
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