The use of solutions to problems of spacecraft trajectory optimization in impulse formulation when solving the problems of optimal control of trajectories of a spacecraft with limited thrust engine: I

✍ Scribed by I. S. Grigoriev; K. G. Grigoriev

• Book ID: 110157632
• Publisher: Springer
• Year: 2007
• Tongue: English
• Weight: 208 KB
• Volume: 45
• Category: Article
• ISSN: 0010-9525
• DOI: 10.1134/s0010952507040077