Design of the Missile Attitude Controller Based on the Active Disturbance Rejection Control

Design of the Missile Attitude Controller Based on the Active Disturbance Rejection Control

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Targeting at the stable tracking control problem of the interceptor missile’s flight attitude in the terminal guidance phase, the nonlinear mathematical model of missile attitude is used as the research object, in which the coupling among the channels is considered. The control strategies of Propor...

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Bibliographic Details
Main Authors: Shanzhong Liu, Mengqi Xue, Yaolong Qiu, Xingyu Zhou, Qingxiu Zhao
Format: Article
Language:English
Published: Instituto de Aeronáutica e Espaço (IAE) 2022-05-01
Series:Journal of Aerospace Technology and Management
Subjects:
attitude control
active disturbance rejection control
extended state observer
robustness
Online Access:https://www.scielo.br/j/jatm/a/P9rvTJ8WPwCycSbnWzzqFSM/?format=pdf&lang=en

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