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Optimization of the spacecraft launch into orbit
| Authors: Gorokhov I.E. | Published: 03.09.2020 |
| Published in issue: #7(48)/2020 | |
| DOI: DOI: 10.18698/2541-8009-2020-7-628 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: optimal control, spacecraft, launch into orbit, pitch angle, boundary value problem, geostationary orbit, Pontryagin’s maximum method, system of differential equations, optimality criterion, launch vehicle | |