Attitude control system conceptual design for the X-ray timing explorer

Details Attitude control system conceptual design for the X-ray timing explorer Attitude control system conceptual design for the X-ray timing explorer

Aug 1992

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992gnc..conf..236b&link_type=abstract

IN: AIAA Guidance, Navigation and Control Conference, Hilton Head Island, SC, Aug. 10-12, 1992, Technical Papers. Pt. 1 (A92-551

Other

Control Systems Design, Satellite Attitude Control, X Ray Timing Explorer, Kalman Filters, Pointing Control Systems, Spacecraft Stability

Scientific paper

The X-ray Timing Explorer (XTE) satellite is the next in a long series of Explorer-class missions developed by NASA. It will study the structure and dynamics of compact X-ray sources, neutron stars, white dwarfs, and other stellar objects with X-ray energy emissions. The demanding pointing requirement of XTE are driving the attitude control system design. This design is further complicated by large moving instruments which impart significant momentum on the spacecraft. The attitude control system concept to meet the XTE science objectives is discussed.

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