Determination of satellite orbit parameters via measurements of the angular position of the satellite from an orbital spacecraft

Details Determination of satellite orbit parameters via measurements of the angular position of the satellite from an orbital spacecraft Determination of satellite orbit parameters via measurements of the angular position of the satellite from an orbital spacecraft

Jan 1992

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992kosis..30...45d&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 30, no. 1, Jan.-Feb. 1992, p. 45-51. In Russian.

Physics

Orbital Elements, Orbital Position Estimation, Satellite Orientation, Spacecraft Control, Spacecraft Orbits, Circular Orbits, Position Errors, Root-Mean-Square Errors

Scientific paper

A method is proposed for determining the orbit parameters of an earth
satellite using angular measurements from a spacecraft that has known
orbit and attitude parameters. It is noted that this method is suitable
for the case of short-duration observations. Formulas for calculating
the rms errors associated with the parameters estimated are presented.

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