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Communication Dans Un Congrès Année : 2001

Time optimal control of a satellite with two rotors

Ugo Boscain
Yacine Chitour

Résumé

The aim of this work is to investigate the structure of time-optimal trajectories for a control system modelizing a satellite with two rotors attached along its two fixed axes. Our results extend to the general case those obtained by Sussmann and Tang in an unpublished paper where they treat a particular case described below. We end up finding a sufficient family of four parameters trajectory types. The main tools used are the Pontryagin Maximum Principle, switching functions and envelope theory. © 2001 EUCA.
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Dates et versions

hal-02320857 , version 1 (19-10-2019)

Identifiants

  • HAL Id : hal-02320857 , version 1

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Ugo Boscain, Yacine Chitour, Benedetto Piccoli. Time optimal control of a satellite with two rotors. 6th European Control Conference, ECC 2001, Sep 2001, Porto, Portugal. pp.1721-1725. ⟨hal-02320857⟩

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