Synthesis of control of descent from satellite orbit of a gliding space vehicle by varying the roll angle

Details Synthesis of control of descent from satellite orbit of a gliding space vehicle by varying the roll angle Synthesis of control of descent from satellite orbit of a gliding space vehicle by varying the roll angle

Publishing date

Jul 1977

URL

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1977cosre..15...28n&link_type=associated

Journals

(Kosmicheskie Issledovaniia, vol. 15, Jan.-Feb. 1977, p. 34-41.) Cosmic Research, vol. 15, no. 1, July 1977, p. 28-34. Translat

Science

Physics

Additional info 3

Descent Trajectories, Lateral Control, Numerical Control, Spacecraft Reentry, Trajectory Optimization, Algorithms, Lift Drag Ratio, Monte Carlo Method, Spacecraft Maneuvers, Time Optimal Control, Winged Vehicles

Type

Scientific paper

Abstract

Not Available

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