Determination of orbits from measurements of angles

Details Determination of orbits from measurements of angles Determination of orbits from measurements of angles

Sep 1974

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1974kosis..12..669s&link_type=abstract

Kosmicheskie Issledovaniia, vol. 12, Sept.-Oct. 1974, p. 669-674. In Russian.

Computer Science

Angular Velocity, Orbital Elements, Orbital Position Estimation, Satellite Orbits, Algorithms, Earth Orbits, Error Analysis, Kepler Laws, Position Errors, Transcendental Functions

Scientific paper

An algorithm is proposed for determining a Keplerian satellite orbit from the values measured for two moments of time, four angular coordinates of two positions, and two angular velocity components. The problem of determining the orbit is reduced to the solution of a system of two transcendental equations. The existence of four solutions of this system of equations is demonstrated. The accuracy of the determination of orbital elements is studied as a function of measurement errors.

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