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  1. No Access

    Article

    Research for Optimal Programs for Controlling the Relative Motion of a Spacecraft with Limited Thrust

    The problem of optimal control of the relative motion of a spacecraft with a finite thrust engine in arbitrary circumcircular orbits using the Pontryagin’s maximum principle is considered. Motion is studied in...

    S. A. Ishkov, G. A. Filippov in Cosmic Research (2023)

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    Article

    Optimization of project-ballistic parameters for low earth orbit spacecraft with propulsion systems with energy storage

    Optimization of project-ballistic parameters of the spacecraft with propulsion systems with energy accumulation during the orbital transfer between low Earth orbits in the non-central gravitational field of th...

    A. A. Khramov, S. A. Ishkov in Russian Aeronautics (Iz VUZ) (2016)