Theoretical Multiple Approach to Solving Synthesis Problems for Unified Control of Spacecraft Orbit Insertion
| Authors: Proletarsky A.V. | Published: 23.01.2015 |
| Published in issue: #1(50)/2003 | |
| DOI: | |
| Category: Control Systems | |
| Keywords: | |
Requirements to systems of the booster motion control are generalized and the feasibility of synthesis of a unified algorithm for the spacecraft orbit insertion is analyzed.
