About one problem of trajectory optimization

Details About one problem of trajectory optimization About one problem of trajectory optimization

Jun 2008

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2008cosre..46..233g&link_type=abstract

Cosmic Research, Volume 46, Issue 3, pp.233-237

Physics

45.10.Db

Scientific paper

The optimization problem for trajectories of spacecraft flight from the Earth to an asteroid is considered in this paper. The flight is realized in the central Newtonian gravitational field of the Sun with a possibility of gravitational maneuvers near planets. Perturbation maneuvers are taken into account using the method of point area of action with a limitation on the flyby altitude. The spacecraft is controlled by changing the value and direction of the engine thrust. The problem is solved taking into account constraints on the launch time, flight duration, and minimum distance to the Sun.

Affiliated with

Also associated with

No associations

Rating

About one problem of trajectory optimization 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 About one problem of trajectory optimization, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and About one problem of trajectory optimization will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFWR-SCP-O-1246370