A novel output redefinition method for nonlinear H∞$$ {H}_{\infty } $$ attitude stabilization of a flexible spacecraft

Author:

Majid Esmaeilzadeh Seyed1ORCID,Sadegh Zeyghami Mohammad1

Affiliation:

1. Electrical Engineering Department Iran University of Science and Technology Tehran Iran

Abstract

AbstractThis paper addresses a novel output redefinition method for the nonlinear attitude stabilization problem of a flexible spacecraft. As an idea, the flexible appendage tip‐point can be selected as attitude output which may improve attitude pointing accuracy. However, it makes the system non‐minimum phase. The output redefinition method is an effective method to make the system minimum phase. In this paper, a novel output redefinition is proposed to overcome the non‐minimum phase property such that it improves the attitude control system performance. Then, a nonlinear controller is designed based on back‐stepping approach and a modal observer. The simulation results show the effectiveness of the proposed method in the presence of model uncertainties and environmental disturbances.

Publisher

Wiley

Subject

Control and Systems Engineering,Electrical and Electronic Engineering,Mathematics (miscellaneous)

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