Robust attitude stabilization of spacecraft using nonlinear quaternion feedback

This paper considers the problem of three-axis attitude stabilization of a rigid spacecraft. A nonlinear control law which uses the feedback of the unit quaternion and the measured angular velocities is proposed and is shown to provide global asymptotic stability. The control law does not require th...

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Published in:IEEE transactions on automatic control 1995-10, Vol.40 (10), p.1800-1803
Main Authors: Joshi, S.M., Kelkar, A.G., Wen, J.T.-Y.
Format: Article
Language:English
Subjects:
Angular velocity
Angular velocity control
Applied sciences
Asymptotic stability
Computer science
control theory
systems
Control system synthesis
Control theory. Systems
Error correction
Exact sciences and technology
Feedback
Quaternions
Robust control
Robustness
Space vehicles
Velocity measurement
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cited_by cdi_FETCH-LOGICAL-c401t-d826a1fc99d54c652d86d422eb962735da7d2de0d034a5a6e565a0f5910341cb3
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container_title IEEE transactions on automatic control
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creator Joshi, S.M.
Kelkar, A.G.
Wen, J.T.-Y.
description This paper considers the problem of three-axis attitude stabilization of a rigid spacecraft. A nonlinear control law which uses the feedback of the unit quaternion and the measured angular velocities is proposed and is shown to provide global asymptotic stability. The control law does not require the knowledge of the system parameters and is, therefore, robust to modeling errors. The significance of the control law is that it can be used for large-angle maneuvers with guaranteed stability.< >
doi_str_mv 10.1109/9.467669
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source IEEE Electronic Library (IEL) Journals
subjects Angular velocity
Angular velocity control
Applied sciences
Asymptotic stability
Computer science
control theory
systems
Control system synthesis
Control theory. Systems
Error correction
Exact sciences and technology
Feedback
Quaternions
Robust control
Robustness
Space vehicles
Velocity measurement
title Robust attitude stabilization of spacecraft using nonlinear quaternion feedback
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