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Communication Dans Un Congrès Année : 2019

Using Differential Flatness for solving the Minimum-Fuel Low-Thrust Geostationary Station-Keeping Problem

Résumé

The minimum fuel station keeping of a geostationary satellite equipped with electric thrusters undergoing the Earth non-spherical disturbing gravitational potential up to degree and order 2 is first recast by transforming the linear time varying relative dynamics in a time invariant one with a Floquet-Lyapunov transformation. In a second step, the flatness property of the system is used to convert the genuine optimal control problem to a linear programming problem. This problem is solved for an ideal geostationary satellite with one thruster mounted on each face.
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Dates et versions

hal-02171917 , version 1 (03-07-2019)

Identifiants

  • HAL Id : hal-02171917 , version 1

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Clément Gazzino, Christophe Louembet. Using Differential Flatness for solving the Minimum-Fuel Low-Thrust Geostationary Station-Keeping Problem. 9th European Conference for Aeronautics and Space Sciences (EUCASS 2019), Jul 2019, Madrid, Spain. ⟨hal-02171917⟩
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