The problem of processing information during controlled descent in the atmosphere

Details The problem of processing information during controlled descent in the atmosphere The problem of processing information during controlled descent in the atmosphere

Jul 1978

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1978kosis..16..467b&link_type=abstract

Kosmicheskie Issledovaniia, vol. 16, July-Aug. 1978, p. 467-474. In Russian.

Physics

Atmospheric Entry, Data Processing, Descent Trajectories, Kalman Filters, Reentry Guidance, Spacecraft Control, Control Theory, Equations Of Motion, Error Analysis, Linearization, Optimal Control, Root-Mean-Square Errors, Spacecraft Landing, Spacecraft Reentry

Scientific paper

Some aspects are discussed of the problem of designing an optimal information processing system for the autonomous control of a spacecraft during the atmospheric phase of reentry at near-orbital velocities. The aim of the control is to achieve a pin-point landing. A method of designing the information processing system on the basis of the Kalman filter is proposed.

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