Single saturated PD control for asymptotic attitude stabilisation of spacecraft-Reference-Cited by-同舟云学术

Single saturated PD control for asymptotic attitude stabilisation of spacecraft

Published:2020-12 Issue:19 Volume:14 Page:3338-3343
ISSN:1751-8644
Container-title:IET Control Theory & Applications
language:en
Short-container-title:IET Control Theory & Appl

Author:

Su Yuxin¹^ORCID,Zheng Chunhong²^ORCID

Affiliation:

1. School of Electro‐Mechanical Engineering, Xidian UniversityXi'an710071People's Republic of China

2. School of Electronic Engineering, Xidian UniversityXi'an710071People's Republic of China

Publisher

Institution of Engineering and Technology (IET)

Subject

Electrical and Electronic Engineering,Control and Optimization,Computer Science Applications,Human-Computer Interaction,Control and Systems Engineering

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1049/iet-cta.2020.0598

Reference30 articles.

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2. Inverse optimal stabilization of a rigid spacecraft;Kristic M.;IEEE Trans. Autom. Control,1999

3. Finite‐time output feedback attitude stabilisation for rigid spacecraft with input constraints;Sun S.H.;IET Control Theory Appl.,2016

4. Rigid‐body attitude stabilization with attitude and angular rate constraints;Shen Q.;Automatica,2018

5. Quaternion feedback regulator for spacecraft eigenaxis rotations;Wie B.;J. Guid. Control Dyn.,1989

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