Disturbance rejection dynamic inverse control of air-breathing hypersonic vehicles

被引:20
作者
An, Hao [1 ]
Wu, Qianqian [2 ]
机构
[1] Harbin Inst Technol, Space Control & Inertial Technol Res Ctr, Res Ctr Satellite Technol, Harbin 150001, Heilongjiang, Peoples R China
[2] Harbin Inst Technol, Ctr Composite Mat & Struct, Harbin 150001, Heilongjiang, Peoples R China
基金
中国博士后科学基金;
关键词
Air-breathing hypersonic vehicle; Control system design; Disturbance rejection; Nonlinear dynamic inverse; TRACKING CONTROL; ADAPTIVE-CONTROL; FLIGHT VEHICLE; CONTROL DESIGN; SYSTEMS;
D O I
10.1016/j.actaastro.2018.06.022
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper presents a disturbance rejection controller for air-breathing hypersonic vehicles (AHVs) based on the technique of nonlinear dynamic inverse (NDI). An observer is employed to estimate the lumped disturbance on the nominal dynamics of AHVs, such as the external disturbances introduced by the changeable flight environment and the unsteady scramjet operation. With the help of this observer, an effective NDI controller is proposed to suppress the negative effect of the lumped disturbance on output channels. Under the proposed control, the input-to-state stability of the closed-loop AHV system can be ensured if the observer gain matrix is properly selected. A simulation study on the disturbed AHV model is provided to illustrate the effectiveness of this disturbance rejection NDI control.
引用
收藏
页码:348 / 356
页数:9
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