The July 2 Earth Radiation Budget Satellite (ERBS) hydrazine thruster-controlled yaw inversion maneuver resulted in a 2.1 deg/sec attitude spin. This mode continued for 150 minutes until the spacecraft was inertially despun using the hydrazine thrusters. The spacecraft remained in a low-rate Y-axis spin of .06 deg/sec for 3 hours until the B-DOT control mode was activated. After 5 hours in this mode, the spacecraft Y-axis was aligned to the orbit normal, and the spacecraft was commanded to the mission mode of attitude control. This work presents the experience of real-time attitude determination support following analysis using the playback telemetry tape recorded for 7 hours from the start of the attitude control anomaly.


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    Titel :

    Attitude analysis of the Earth Radiation Budget Satellite (ERBS) yaw turn anomaly


    Beteiligte:


    Erscheinungsdatum :

    01.09.1988


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Attitude Analysis of the Earth Radiation Budget Satellite (ERBS) Yaw Turn Anomaly

    J. Kronenwetter / M. Phenneger / W. L. Weaver | NTIS | 1988


    Earth Radiation Budget Satellite (ERBS): Emergency Support

    J. Williamson / P. Pashby | NTIS | 1991


    In-orbit Earth Radiation Budget Satellite (ERBS) Battery Switch

    Ahmad, A. / Enciso, M. / Rao, G. et al. | British Library Conference Proceedings | 2000


    In-Orbit Earth Radiation Budget Satellite (ERBS) Battery Switch

    Ahmad, Anisa / Enciso, Marlon / Rao, Gopalakrishna | NTRS | 2000