Optimization of passive orbit with the use of gravity maneuver

Details Optimization of passive orbit with the use of gravity maneuver Optimization of passive orbit with the use of gravity maneuver

Oct 2008

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2008cosre..46..456s&link_type=abstract

Cosmic Research, Volume 46, Issue 5, pp.456-464

Physics

45.40.Gj

Scientific paper

A high-precision method of calculating gravitational interactions is applied in order to determine optimal trajectories. A number of problems, necessary for determination of optimal parameters at a launch of a spacecraft and during its flyby near celestial bodies, are considered. The spacecraft trajectory was determined by numerical integration of the equations of passive motion of the spacecraft and of the equations of motion for planets, the Sun, and the Moon. The optimal trajectory of the spacecraft approaching the Sun is determined by fitting its initial conditions.

Affiliated with

Also associated with

No associations

Rating

Optimization of passive orbit with the use of gravity maneuver does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.

If you have personal experience with Optimization of passive orbit with the use of gravity maneuver, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Optimization of passive orbit with the use of gravity maneuver will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFWR-SCP-O-1699303