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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Bibliographic Details

Published in:	علوم، فناوری و کاربردهای فضایی
Main Authors:	Sayyed Mohammad Mousavi, Sayyed Majid Esmailifar, Mohammad Chiniforoushan
Format:	Article
Language:	Persian
Published:	Iranian Space Research Institute 2022-02-01
Subjects:	time optimal control# attitude and position dynamics# orbital rendezvous maneuver# pseudospectral method# bang bang control structure
Online Access:	https://journal.isrc.ac.ir/article_146952_4001fae556e11265709e8d78ebbece42.pdf