Dynamic Modeling and Active Morphing Trajectory-Attitude Separation Control Approach for Gull-Wing Aircraft

被引：24

作者：

Guo, Tianhao ^{[1
]}

Hou, Zhongxi ^{[1
]}

Zhu, Bingjie ^{[1
]}

机构：

[1] Natl Univ Def Technol, Coll Aerosp Sci & Engn, Changsha 410073, Hunan, Peoples R China

来源：

IEEE ACCESS | 2017年 / 5卷

基金：

美国国家科学基金会;

关键词：

Morphing aircraft; centroid dynamic equations; linear parameter varying (LPV); controller synthesis; H-infinity control; SIMULATION; DESIGN;

D O I：

10.1109/ACCESS.2017.2743059

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Morphings are usually used for aircrafts to achieve a better performance in variable environment, whereas this paper focuses on how to achieve a trajectory-attitude separation control effect with an active morphing strategy. Aimed at this target, a systemic work, including modeling, linearization, and control, is presented. An accurate nonlinear dynamic model of morphing aircraft is built with centroid dynamic equations, of which all the additional terms that stem from morphing are expatiated for gull wing aircraft. Then, a linear parameter varying (LPV) approach is applied to linearize the equations for a controller design. A state feedback with a feedforward H-infinity control approach for an LPV system is proposed in this paper and is applied to the attitude control of gull-wing aircraft. Based on the stabilized aircraft attitude, a dynamic inversion control approach for the trajectory channels with active morphing is designed. The nonlinear simulation cases validate the feasibility of trajectory-attitude separation control with active morphing, as well as the performance of the control approach proposed in this paper.

引用

页码：17006 / 17019

页数：14