Optimum program of control of continuous low-thrust at flight between noncoplanar elliptical and geostationary orbits
2018
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.
- Correction
- Source
- Cite
- Save
- Machine Reading By IdeaReader
1
References
0
Citations
NaN
KQI