Time-optimal Control of Spacecraft Rotational and Translational Dynamics in Orbital Rendezvous Maneuver

Sayyed Mohammad Mousavi; Sayyed Majid Esmailifar; Mohammad Chiniforoushan

Volume 1, Issue 2 , March 2022, , Pages 147-166

  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 actuators ...  Read More