Optimization of closed low-thrust Earth-Mars-Earth flights.

Details Optimization of closed low-thrust Earth-Mars-Earth flights. Optimization of closed low-thrust Earth-Mars-Earth flights.

Apr 1995

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1995kosis..33..210i&link_type=abstract

Kosmicheskie Issledovaniia, Tom 33, No. 2, p. 210 - 219

Statistics

Computation

Space Missions: Mars, Space Missions: Orbits

Scientific paper

The problem of optimization of the trajectory and ballistic parameters of a low-thrust interplanetary Earth-Mars-Earth flight is formulated. A methodical approach to solve the optimization problem under constraints on the spacecraft launching mass, flight duration, and minimal heliocentric distance is proposed. The algorithm considered is based on a combination of the Pontryagin maximum principle and mathematical programming methods. For computation of the heliocentric stages of flight, approximate analytical relationships obtained from the results of the solution of a set of variation problems are used. For a closed flight, rational ballistic schemes that satisfy the totality of constraints are selected.

Affiliated with

Also associated with

No associations

Rating

Optimization of closed low-thrust Earth-Mars-Earth flights. 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 closed low-thrust Earth-Mars-Earth flights., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Optimization of closed low-thrust Earth-Mars-Earth flights. will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFWR-SCP-O-1830295