Inertial coordinate representation of mission analysis problems

Details Inertial coordinate representation of mission analysis problems Inertial coordinate representation of mission analysis problems

Feb 1986

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1986jspro..23..118k&link_type=abstract

Journal of Spacecraft and Rockets (ISSN 0022-4650), vol. 23, Jan.-Feb. 1986, p. 118, 119.

Physics

Inertial Coordinates, Mission Planning, Satellite Attitude Control, Spaceborne Telescopes, Satellite Rotation, Sensors, Spheres

Scientific paper

In the present method for the application of celestial coordinates to attitude sensor problems, the coupling of spacecraft orbit and sensor geometry normally obtained through classical coordinate transformations is uniquely represented by a global picture. Relative directions are plotted as if the spacecraft were located at the center of the celestial sphere. The technique is applied to the attitude determination of a communication satellite and the mission planning of a space telescope.

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