We suggest a determined iterative algorithm of defining the planar parameters of a spacecraft Keplerian orbit in the velocity reference frame. Analytical relations for creating the iterative algorithm and the numeric example of defining parameters of a spacecraft Keplerian orbit are given.
Onboard Iterative Algorithm of Defining the Parameters of Keplerian Orbits Based on Solving the Orbital Motion Equations in Velocity Reference Frame
Russ. Aeronaut.
Russian Aeronautics ; 64 , 3 ; 432-440
2021-07-01
9 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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