Discussion on the paper "Optimal Magnetic Momentum Control for Inertially Pointing Spacecraft"

Publikation: Bidrag til tidsskriftTidsskriftartikelFormidling

Resumé

The paper by Maro Lovera proposes a novel momentum unloading algorithm for an inertially stabilized spacecraft. The spacecraft is actuated by reaction wheels working in zero momentum bias. The periodic control theory is used for synthesis of a controller compensating external disturbances by means of reaction wheels and magnetic actuators. The key issue is an observation that the magnetic field as observed from a low earth orbit is almost periodic
OriginalsprogDansk
TidsskriftEuropean Journal of Control
Vol/bind7
Udgave nummer1
Sider (fra-til)40-42
ISSN0947-3580
StatusUdgivet - 2001

Citer dette

@article{20e51080001f11dab4d5000ea68e967b,
title = "Discussion on the paper {"}Optimal Magnetic Momentum Control for Inertially Pointing Spacecraft{"}",
abstract = "The paper by Maro Lovera proposes a novel momentum unloading algorithm for an inertially stabilized spacecraft. The spacecraft is actuated by reaction wheels working in zero momentum bias. The periodic control theory is used for synthesis of a controller compensating external disturbances by means of reaction wheels and magnetic actuators. The key issue is an observation that the magnetic field as observed from a low earth orbit is almost periodic",
author = "Rafal Wisniewski",
year = "2001",
language = "Dansk",
volume = "7",
pages = "40--42",
journal = "European Journal of Control",
issn = "0947-3580",
publisher = "Elsevier",
number = "1",

}

Discussion on the paper "Optimal Magnetic Momentum Control for Inertially Pointing Spacecraft". / Wisniewski, Rafal.

I: European Journal of Control, Bind 7, Nr. 1, 2001, s. 40-42.

Publikation: Bidrag til tidsskriftTidsskriftartikelFormidling

TY - JOUR

T1 - Discussion on the paper "Optimal Magnetic Momentum Control for Inertially Pointing Spacecraft"

AU - Wisniewski, Rafal

PY - 2001

Y1 - 2001

N2 - The paper by Maro Lovera proposes a novel momentum unloading algorithm for an inertially stabilized spacecraft. The spacecraft is actuated by reaction wheels working in zero momentum bias. The periodic control theory is used for synthesis of a controller compensating external disturbances by means of reaction wheels and magnetic actuators. The key issue is an observation that the magnetic field as observed from a low earth orbit is almost periodic

AB - The paper by Maro Lovera proposes a novel momentum unloading algorithm for an inertially stabilized spacecraft. The spacecraft is actuated by reaction wheels working in zero momentum bias. The periodic control theory is used for synthesis of a controller compensating external disturbances by means of reaction wheels and magnetic actuators. The key issue is an observation that the magnetic field as observed from a low earth orbit is almost periodic

M3 - Tidsskriftartikel

VL - 7

SP - 40

EP - 42

JO - European Journal of Control

JF - European Journal of Control

SN - 0947-3580

IS - 1

ER -