The problem of the formation of an optimal control program spacecraft with low thrust at flight between the noncoplanar elliptical and geostationary orbits is considered. A scheme for the joint change of orbital elements within the simple structure of the thrust vector control on the circuit is offered.
Optimum program of control of continuous low-thrust at flight between noncoplanar elliptical and geostationary orbits
ICNPAA 2018 WORLD CONGRESS: 12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences ; 2018 ; Yerevan, Armenia
AIP Conference Proceedings ; 2046 , 1
04.12.2018
6 pages
Aufsatz (Konferenz)
Elektronische Ressource
Englisch