Quaternion Feedback Control for Rigid-body Spacecraft

Hans-Christian Becker Jensen; Rafal Wisniewski

Quaternion Feedback Control for Rigid-body Spacecraft

Hans-Christian Becker Jensen, Rafal Wisniewski

Publikation: Bidrag til bog/antologi/rapport/konference proceeding › Konferenceartikel i proceeding › Forskning

Abstract

This paper addresses three-axis attitude control for a Danish spacecraft, Roemer. The algorithm proposed is based on an approximation of the exact feedback linearisation for quaternionic attitude representation. The proposed attitude controller is tested in a simulation study. The environmental disturbances correspond to those expected for the Roemer mission. The pros and cons of the algorithm are discussed. The results of the study show that the controller is a successful candidate for on-board implementation

Originalsprog	Dansk
Titel	Guidance, Navigation, and Control Conference, 6-9 August 2001, Montréal, Québec Canada
Publikationsdato	2001
Status	Udgivet - 2001
Begivenhed	Quaternion Feedback Control for Rigid-body Spacecraft - Varighed: 19 maj 2010 → …

Konference

Konference	Quaternion Feedback Control for Rigid-body Spacecraft
Periode	19/05/2010 → …

AUB Link

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Citationsformater

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title = "Quaternion Feedback Control for Rigid-body Spacecraft",

abstract = "This paper addresses three-axis attitude control for a Danish spacecraft, Roemer. The algorithm proposed is based on an approximation of the exact feedback linearisation for quaternionic attitude representation. The proposed attitude controller is tested in a simulation study. The environmental disturbances correspond to those expected for the Roemer mission. The pros and cons of the algorithm are discussed. The results of the study show that the controller is a successful candidate for on-board implementation",

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AB - This paper addresses three-axis attitude control for a Danish spacecraft, Roemer. The algorithm proposed is based on an approximation of the exact feedback linearisation for quaternionic attitude representation. The proposed attitude controller is tested in a simulation study. The environmental disturbances correspond to those expected for the Roemer mission. The pros and cons of the algorithm are discussed. The results of the study show that the controller is a successful candidate for on-board implementation

M3 - Konferenceartikel i proceeding

BT - Guidance, Navigation, and Control Conference, 6-9 August 2001, Montréal, Québec Canada

T2 - Quaternion Feedback Control for Rigid-body Spacecraft

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