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Development and Laboratory Verification of Control Algorithms for Formation Flying Configuration with a Single-Input Impulsive Control

Ovchinnikov, M. Y. und Bindel, D. und Ivanov, D. S. und Smirnov, G. V. und Theil, S. und Zaramenskikh, I. E. (2009) Development and Laboratory Verification of Control Algorithms for Formation Flying Configuration with a Single-Input Impulsive Control. In: Proceedings of the 60th International Astronautical Conference IAC 2009, October 12-16, Daejeong, Korea. International Austronautical Congress, 12. - 16. Okt. 2009, Daejeon, Korea.

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Kurzfassung

Once been orbited, the technological nanosatellite TNS-0 is supposed to be used in one of the next missions for the demonstration of orbital maneuvering capability to eliminate a secular relative motion of two satellites due to J2 harmonic of the Earth’s gravitational field. It is assumed that the longitudinal axis of the satellite is stabilized along the induction vector of the geomagnetic field and a thruster engine is installed along this axis. Continuous and impulse thruster control algorithms eliminating the secular relative motion have been developed. For demonstration and laboratory testing of the satellite motion identification and control algorithms, special equipment was developed in ZARM. The facility consists of a horizontal smooth table and mobile mock-up that enables to glide over the table surface due to compressed air stored in on-board pressure tank. Compressed air is used to control the translation and attitude motion of the mock-up equipped with a number of pulse thrusters. In this work a dynamical model for mock-up controlled motion over the table is developed. This allows to simulate a relative motion of pair of TNS-0 type nanosatellites in the plane of the orbit.

Dokumentart:Konferenzbeitrag (Paper)
Titel:Development and Laboratory Verification of Control Algorithms for Formation Flying Configuration with a Single-Input Impulsive Control
Autoren:
AutorenInstitution oder E-Mail-Adresse der Autoren
Ovchinnikov, M. Y.Keldysh Institute of Applied Mathematics of RAS
Bindel, D.Center of Applied Space Technology and Microgravity, Bremen University
Ivanov, D. S.Keldysh Institute of Applied Mathematics of RAS
Smirnov, G. V.Centro de Matematica da Universidade do Porto, Universidade do Porto
Theil, S.Stephan.Theil@dlr.de
Zaramenskikh, I. E.Keldysh Institute of Applied Mathematics of RAS
Datum:12 Oktober 2009
Erschienen in:Proceedings of the 60th International Astronautical Conference IAC 2009, October 12-16, Daejeong, Korea
Referierte Publikation:Nein
In ISI Web of Science:Nein
Status:veröffentlicht
Stichwörter:Impulsive control, orbit control, onground simulation
Veranstaltungstitel:International Austronautical Congress
Veranstaltungsort:Daejeon, Korea
Veranstaltungsart:internationale Konferenz
Veranstaltungsdatum:12. - 16. Okt. 2009
Veranstalter :International Astronautical Federation
HGF - Forschungsbereich:Verkehr und Weltraum (alt)
HGF - Programm:Weltraum (alt)
HGF - Programmthema:W - keine Zuordnung
DLR - Schwerpunkt:Weltraum
DLR - Forschungsgebiet:W - keine Zuordnung
DLR - Teilgebiet (Projekt, Vorhaben):W -- keine Zuordnung (alt)
Standort: Bremen
Institute & Einrichtungen:Institut für Raumfahrtsysteme > Regelungs- und Datensysteme
Hinterlegt von: Dr.-Ing. Stephan Theil
Hinterlegt am:04 Jan 2010 15:08
Letzte Änderung:12 Dez 2013 20:45

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