Physics
Scientific paper
Jul 1994
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1994iscjs...4...36t&link_type=abstract
In ISRO Satellite Centre, Journal of Spacecraft Technology, Volume 4, No . 2, July 1994 p 36-42 (SEE N95-13825 03-12)
Physics
Attitude (Inclination), Field Of View, Indian Spacecraft, Instrument Orientation, Remote Sensing, Satellite Observation, Stabilized Platforms, Star Trackers, Charge Coupled Devices, Microprocessors, Optical Equipment, Polar Orbits, Skewness, Synchronous Satellites
Scientific paper
A microprocessor-based star sensor system using an array Charge Coupled Device (CCD) as detector has been developed for the attitude determination of Indian Remote Sensing Satellites IRS 1C & 1D. A pair of sensors with Field of View (FOV) of 8 deg x 6 deg, mounted in skewed configuration in the 3-axis stabilized satellite platform, capable of detecting stars up to 5.0 visual magnitude (Mv) can give an attitude determination accuracy of better than 0.01 deg.
Jain Y. K.
Koteswara Rao V.
Pratap G.
Rao Goparaju Nagendra
Thomas Philip
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