Optimal reorientation of a spacecraft with reversible motor

Details Optimal reorientation of a spacecraft with reversible motor Optimal reorientation of a spacecraft with reversible motor

May 1975

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1975kosis..13..427l&link_type=abstract

Kosmicheskie Issledovaniia, vol. 13, May-June 1975, p. 427-430. In Russian.

Physics

Jet Thrust, Maneuverable Spacecraft, Optimal Control, Spacecraft Stability, Thrust Vector Control, Fuel Consumption, Thrust Programming, Thrust Reversal

Scientific paper

Solution of the problem of bringing a space vehicle into a state of
stabilized rotation in a given direction in inertial space, where the
control moment is provided by a reversible orientation jet engine.
Quality criterion is fuel expenditure. Two engine firings are necessary
for the procedure.

Affiliated with

Also associated with

No associations

Rating

Optimal reorientation of a spacecraft with reversible motor 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 Optimal reorientation of a spacecraft with reversible motor, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Optimal reorientation of a spacecraft with reversible motor will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFWR-SCP-O-1049263