A method for operational control of satellite motion during its descent into the atmosphere

Details A method for operational control of satellite motion during its descent into the atmosphere A method for operational control of satellite motion during its descent into the atmosphere

Mar 1991

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1991kosis..29..238m&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 29, Mar.-Apr. 1991, p. 238-246. In Russian.

Mathematics

Atmospheric Entry, Descent Trajectories, Reusable Spacecraft, Spacecraft Maneuvers, Trajectory Control, Ground Stations, Real Time Operation, Terminal Ballistics

Scientific paper

A method is proposed for on-ground trajectory control of a reusable spacecraft (such as the Soviet shuttle Buran or the U.S. Space Shuttle) during its descent into the atmosphere. Both the standard-program and the return-to-launch-site cases are considered. The guaranteed and the probable boundaries of the admissible-region maneuver are presented. Using results of mathematical simulations, a data base of boundary constraints is developed for use in the satellite-motion control.

Affiliated with

Also associated with

No associations

Rating

A method for operational control of satellite motion during its descent into the atmosphere 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 A method for operational control of satellite motion during its descent into the atmosphere, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and A method for operational control of satellite motion during its descent into the atmosphere will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFWR-SCP-O-1606001