New one-axis one-sensor magnetic attitude control theoretical and in-flight performance

New one-axis one-sensor magnetic attitude control theoretical and in-flight performance

New one-axis magnetic attitude control is proposed. Only one attitude sensor providing any inertial direction measurements is necessary, magnetometer is not used. The control may be used as a backup capability in case main actuators or some attitude sensors fail. Sun pointing is achievable using onl...

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Veröffentlicht in:Acta astronautica 2014-12, Vol.105 (1), p.12-16
Hauptverfasser: Ovchinnikov, MYu, Roldugin, D S, Tkachev, S S, Karpenko, SO
Format: Artikel
Sprache:eng
Schlagworte:
Actuators
Asymptotic properties
Attitude control
Inertia
Mathematical analysis
Power consumption
Sensors
Sun
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container_title Acta astronautica
container_volume 105
creator Ovchinnikov, MYu
Roldugin, D S
Tkachev, S S
Karpenko, SO
description New one-axis magnetic attitude control is proposed. Only one attitude sensor providing any inertial direction measurements is necessary, magnetometer is not used. The control may be used as a backup capability in case main actuators or some attitude sensors fail. Sun pointing is achievable using only three-axis Sun sensor, so the control may be used to lower the power consumption during battery charging. Asymptotic stability of different equilibria depending on the satellite inertia tensor is summarized. In-flight results from "Chibis-M" microsatellite are provided proving general control performance.
doi_str_mv 10.1016/j.actaastro.2014.08.017
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source Elsevier ScienceDirect Journals
subjects Actuators
Asymptotic properties
Attitude control
Inertia
Mathematical analysis
Power consumption
Sensors
Sun
title New one-axis one-sensor magnetic attitude control theoretical and in-flight performance
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