Recurrent-iterative algorithm for control synthesis of spacecraft terminal reorientation based on the method for analytical design of optimal controllers
Published: 24.09.2021
Authors: Pushkar O.D.
Published in issue: #9(117)/2021
DOI: 10.18698/2308-6033-2021-9-2112
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control