A new procedure for the solution of the classical problem of minimal orbit determination from three lines of sight

Author:

Gooding R. H.

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Astronomy and Astrophysics,Applied Mathematics,Computational Mathematics,Mathematical Physics,Modelling and Simulation

Reference19 articles.

1. Brouwer, D. and Ashbrook, J.: 1951, ?The Minor Planet (619) Triberga and the Mass of the Moon?, Astron. J. 56, 57.

2. Briggs, R. E. and Slowey, J. W.: 1959, ?An Iterative Method of Orbit Determination from Three Observations of a Nearby Satellite?, Smiths, Inst. Astron. Obs., Special Report 27.

3. Escobal, P. R.: 1965 (and 1985), Methods of Orbit Determination, Wiley, New York (and Krieger, Malabar).

4. Gooding, R. H.: 1988, ?On Universal Elements and Conversion Procedures to and from Position and Velocity?, Celest. Mech. 44 283?298.

5. Gooding, R. H. and Odell, A. W.: 1988: ?The Hyperbolic Kepler Equation (and the Elliptic Equation revisited)?, Celest. Mech. 44, 267?282.

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