Algorithm for the terminal control of spacecraft descent in the earth's atmosphere with a low lift-drag ratio

Details Algorithm for the terminal control of spacecraft descent in the earth's atmosphere with a low lift-drag ratio Algorithm for the terminal control of spacecraft descent in the earth's atmosphere with a low lift-drag ratio

Jul 1988

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1988kosis..26..542i&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 26, July-Aug. 1988, p. 542-549. In Russian.

Physics

Descent Trajectories, Earth Atmosphere, Lift Drag Ratio, Radio Control, Spacecraft Reentry, Differential Equations, Satellite Attitude Control, Trajectory Control

Scientific paper

An analysis is made of the characteristics of the radio control of spacecraft descent with a lift-drag ratio of 0.2-0.3 after the establishment of radio communication with the earth. Attention is given to a multistep terminal-control algorithm for determining the current values of the parameters of the spacecraft attainability zone and control values with constraints on the maximum loading and bank characteristics. Numerical results are presented.

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