Adaptive algorithms for the control of the descent of a spacecraft in the earth's atmosphere with a large lift-drag ratio

Details Adaptive algorithms for the control of the descent of a spacecraft in the earth's atmosphere with a large lift-drag ratio Adaptive algorithms for the control of the descent of a spacecraft in the earth's atmosphere with a large lift-drag ratio

May 1981

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1981kosis..19..359b&link_type=abstract

Kosmicheskie Issledovaniia, vol. 19, May-June 1981, p. 359-366. In Russian.

Computer Science

Adaptive Control, Atmospheric Entry, Earth Atmosphere, Lift Drag Ratio, Spacecraft Control, Terminal Guidance, Aerodynamic Characteristics, Algorithms, Steepest Descent Method

Scientific paper

An investigation is presented of the descent of a spacecraft with a large lift-drag ratio in the earth's atmosphere; it is assumed that the spacecraft is controlled with respect to roll angle, and side maneuver is taken into account. An analysis is presented of adaptive algorithms for the autonomous terminal guidance with prediction of the ultimate state of the motion. The efficiency of these algorithms in compensating deviations from the prescribed place of landing is evaluated.

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