Attitude Control by Asymmetric Thrusters' Independent off Modulation during Orbit Adjustment Maneuvers

Attitude Control by Asymmetric Thrusters' Independent off Modulation during Orbit Adjustment Maneuvers

A thrusters modulation method is suggested for spacecraft attitude control with asymmetric configured thrusters during orbit adjustment maneuvers. Attitude is controlled by thrusters off-modulation during orbit maneuvers. Usual control method for symmetric configured thrusters can not be applied for...

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Bibliographic Details
Main Author: Hwa-Suk Oh
Format: Article
Language:English
Published: Korean Space Science Society (KSSS) 1999-12-01
Series:Journal of Astronomy and Space Sciences
Online Access:http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/1999/v16n2/OJOOBS_1999_v16n2_265.pdf
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spelling doaj-f455680f892843199dabd204d206983a2020-11-25T01:14:12ZengKorean Space Science Society (KSSS)Journal of Astronomy and Space Sciences2093-55872093-14091999-12-01162265272Attitude Control by Asymmetric Thrusters' Independent off Modulation during Orbit Adjustment ManeuversHwa-Suk Oh0Aerospace Engineering Department, Hankuk Aviation UniversityA thrusters modulation method is suggested for spacecraft attitude control with asymmetric configured thrusters during orbit adjustment maneuvers. Attitude is controlled by thrusters off-modulation during orbit maneuvers. Usual control method for symmetric configured thrusters can not be applied for asymmetric configured thrusters. Disturbance induced from thrusters asymmetricity shall be compensated during pulsing. In this paper, a thrusters control method using null solution is suggested, which is shown working well without inducing disturbance.http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/1999/v16n2/OJOOBS_1999_v16n2_265.pdf
collection DOAJ
language English
format Article
sources DOAJ
author Hwa-Suk Oh
spellingShingle Hwa-Suk Oh
Attitude Control by Asymmetric Thrusters' Independent off Modulation during Orbit Adjustment Maneuvers
Journal of Astronomy and Space Sciences
author_facet Hwa-Suk Oh
author_sort Hwa-Suk Oh
title Attitude Control by Asymmetric Thrusters' Independent off Modulation during Orbit Adjustment Maneuvers
title_short Attitude Control by Asymmetric Thrusters' Independent off Modulation during Orbit Adjustment Maneuvers
title_full Attitude Control by Asymmetric Thrusters' Independent off Modulation during Orbit Adjustment Maneuvers
title_fullStr Attitude Control by Asymmetric Thrusters' Independent off Modulation during Orbit Adjustment Maneuvers
title_full_unstemmed Attitude Control by Asymmetric Thrusters' Independent off Modulation during Orbit Adjustment Maneuvers
title_sort attitude control by asymmetric thrusters' independent off modulation during orbit adjustment maneuvers
publisher Korean Space Science Society (KSSS)
series Journal of Astronomy and Space Sciences
issn 2093-5587
2093-1409
publishDate 1999-12-01
description A thrusters modulation method is suggested for spacecraft attitude control with asymmetric configured thrusters during orbit adjustment maneuvers. Attitude is controlled by thrusters off-modulation during orbit maneuvers. Usual control method for symmetric configured thrusters can not be applied for asymmetric configured thrusters. Disturbance induced from thrusters asymmetricity shall be compensated during pulsing. In this paper, a thrusters control method using null solution is suggested, which is shown working well without inducing disturbance.
url http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/1999/v16n2/OJOOBS_1999_v16n2_265.pdf
work_keys_str_mv AT hwasukoh attitudecontrolbyasymmetricthrustersindependentoffmodulationduringorbitadjustmentmaneuvers
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