Rotational motion control of a spacecraft

Rafal Wisniewski, P. Kulczycki

Publikation: Bidrag til tidsskriftTidsskriftartikelFormidling

16 Citationer (Scopus)

Resumé

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
OriginalsprogDansk
TidsskriftIEEE Transactions on Automatic Control
Vol/bind48
Udgave nummer4
Sider (fra-til)643-646
ISSN0018-9286
StatusUdgivet - 2003

Citer dette

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Rotational motion control of a spacecraft. / Wisniewski, Rafal; Kulczycki, P.

I: IEEE Transactions on Automatic Control, Bind 48, Nr. 4, 2003, s. 643-646.

Publikation: Bidrag til tidsskriftTidsskriftartikelFormidling

TY - JOUR

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AU - Kulczycki, P.

PY - 2003

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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

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SP - 643

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JO - I E E E Transactions on Automatic Control

JF - I E E E Transactions on Automatic Control

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