Properties are investigated of optimum processes of flight control of spacecraft when complete information about motion is available and when control is produced with the purpose of maintaining given values of certain functionals of the trajectory. Such functionals can be parameters of the trajectory characterizing conditions of encounter with a planet or another apparatus in outer space, or parameters determining spatial position of apparatus at a fixed moment of time.
Optimization of Flight Control of Spacecraft
1965
2 pages
Report
No indication
English
Flight control for manned spacecraft
Engineering Index Backfile | 1963
|Engineering Index Backfile | 1959
|Flight Mission Control for Multiple Spacecraft
NTIS | 1990
|NTIS | 1991
|NTIS | 1981
|