An optimal spacecraft trajectory correction method is examined. The method consists of determining the optimal energetics and strategy for interplanetary spacecraft trajectory correction. Calculations for the Earth-Jupiter flight trajectory are presented. (Author)
Method of Determining Optimal Spacecraft Trajectory Correction
1974
14 pages
Report
No indication
English
Trajectory correction of the Spektr-R spacecraft motion
Springer Verlag | 2014
|Trajectory correction of the Spektr-R spacecraft motion
Online Contents | 2014
|NTRS | 1980
|Optimal attitude trajectory planning method for CMG actuated spacecraft
SAGE Publications | 2018
|Optimal attitude trajectory planning method for CMG actuated spacecraft
Online Contents | 2017
|