L_1 adaptive controller design for hypersonic formation flight

作     者：CHEN Qi WAN Jing AI JianLiang 

作者机构：Department of Aeronautics and Astronautics Fudan University Institute of Vehicle Design Fudan University 

出 版 物：《Science China(Technological Sciences)》 (中国科学（技术科学英文版）)

年 卷 期：2016年第59卷第10期

页      码：1597-1608页

摘      要：The design of an L_1 adaptive controller for hypersonic formation flight is presented. The traditional leader/wingman formation control problem is considered, with focused attention on dealing with the input disturbance and parametric variations, both of which are intrinsic properties of the system that result in undesired control performance. A proportional-derivative control scheme based on nonlinear dynamic inversion is implemented as the baseline controller, and an L_1 adaptive controller is augmented to the baseline controller to attenuate the effects of input disturbance and parametric variations. Simulation results illustrate the effectiveness of the proposed control scheme.

主 题 词：hypersonic flight control nonlinear dynamic inversion L1 adaptive control input disturbance parametric variation 

学科分类：08[工学] 081105[081105] 0811[工学-水利类] 

核心收录：

D　O　I：10.1007/s11431-016-0009-9

馆 藏 号：203194435...