Time-optimal Control of Spacecraft Rotational and Translational Dynamics in Orbital Rendezvous Maneuver
In this research, the time-optimal 6 degrees of freedom (6DOF) orbital rendezvous maneuver problem for an inertially asymmetric rigid spacecraft with independent attitude and position control actuators has been investigated. It is also assumed that the spacecraft is equipped with the thruster actuat...
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| Hoofdauteurs: | , , |
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| Formaat: | Artigo |
| Taal: | Persa |
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Iranian Space Research Institute
2022-02-01
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| Reeks: | علوم، فناوری و کاربردهای فضایی |
| Onderwerpen: | |
| Online toegang: | https://journal.isrc.ac.ir/article_146952_4001fae556e11265709e8d78ebbece42.pdf |
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