Rotational motion control of a spacecraft

Rafal Wisniewski; P. Kulczycki

Rotational motion control of a spacecraft

Research output: Contribution to journal › Journal article › Communication

Abstract

The paper adopts the energy shaping method to control of rotational motion. A global representation of the rigid body motion is given in the canonical form by a quaternion and its conjugate momenta. A general method for motion control on a cotangent bundle to the 3-sphere is suggested. The design algorithm is validated for three-axis spacecraft attitude control.
Udgivelsesdato: APR

Original language	Danish
Journal	IEEE Transactions on Automatic Control
Volume	48
Issue number	4
Pages (from-to)	643-646
ISSN	0018-9286
Publication status	Published - 2003

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title = "Rotational motion control of a spacecraft",

abstract = "The paper adopts the energy shaping method to control of rotational motion. A global representation of the rigid body motion is given in the canonical form by a quaternion and its conjugate momenta. A general method for motion control on a cotangent bundle to the 3-sphere is suggested. The design algorithm is validated for three-axis spacecraft attitude control. Udgivelsesdato: APR",

author = "Rafal Wisniewski and P. Kulczycki",

year = "2003",

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pages = "643--646",

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T1 - Rotational motion control of a spacecraft

AU - Wisniewski, Rafal

AU - Kulczycki, P.

PY - 2003

Y1 - 2003

N2 - The paper adopts the energy shaping method to control of rotational motion. A global representation of the rigid body motion is given in the canonical form by a quaternion and its conjugate momenta. A general method for motion control on a cotangent bundle to the 3-sphere is suggested. The design algorithm is validated for three-axis spacecraft attitude control. Udgivelsesdato: APR

AB - The paper adopts the energy shaping method to control of rotational motion. A global representation of the rigid body motion is given in the canonical form by a quaternion and its conjugate momenta. A general method for motion control on a cotangent bundle to the 3-sphere is suggested. The design algorithm is validated for three-axis spacecraft attitude control. Udgivelsesdato: APR

M3 - Tidsskriftartikel

SN - 0018-9286

VL - 48

SP - 643

EP - 646

JO - IEEE Transactions on Automatic Control

JF - IEEE Transactions on Automatic Control

IS - 4

ER -