Application of the recurrent method of parabolic approximation of extremals to the problem of optimal spacecraft behaviour.

Details Application of the recurrent method of parabolic approximation of extremals to the problem of optimal spacecraft behaviour. Application of the recurrent method of parabolic approximation of extremals to the problem of optimal spacecraft behaviour.

Jan 1991

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1991cosre..28..437v&link_type=abstract

Cosmic Res., Vol. 28, No. 4, p. 437 - 444

Physics

Space Vehicles: Encounters

Scientific paper

A recurrent method is developed for the approximation of the extremals, determining the behavior of a dynamic system at the fast transition from a given initial phase state into a final one, taking into accout the constraints on the motion characteristics of the systems. On the basis of a modification of the one-dimensional Pontryagin regulator to a two-dimensional system, one obtains the solution of the problem of spacecraft-satellite rendezvous.

Affiliated with

Also associated with

No associations

Rating

Application of the recurrent method of parabolic approximation of extremals to the problem of optimal spacecraft behaviour. 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 Application of the recurrent method of parabolic approximation of extremals to the problem of optimal spacecraft behaviour., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Application of the recurrent method of parabolic approximation of extremals to the problem of optimal spacecraft behaviour. will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFWR-SCP-O-1895225