Telemetry recovery and uplink commanding of a spacecraft prior to three-axis attitude stabilization

After separation from the launch vehicle, a spacecraft's guidance and control system typically orients the spacecraft autonomously into a three-axis stabilized attitude for non-spinners. If an anomaly occurs, or if the spacecraft fails to orient itself appropriately, the Mission Operations team...

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Bibliographic Details

Published in:	2006 IEEE Aerospace Conference p. 11 pp.
Main Authors:	Bruzzi, J.R., Jensen, J.R., Fielhauer, K.B., Royster, D.W., Srinivasan, D.K.
Format:	Conference Proceeding
Language:	English
Published:	IEEE 2006
Subjects:	Attitude control Command and control systems Control systems Mobile robots Navigation Receiving antennas Remotely operated vehicles Satellite ground stations Space vehicles Telemetry
Online Access:	Get full text
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