Approximate solution of the filtering problem for spacecraft control in an atmosphere

Details Approximate solution of the filtering problem for spacecraft control in an atmosphere Approximate solution of the filtering problem for spacecraft control in an atmosphere

Nov 1980

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1980kosis..18..844b&link_type=abstract

Kosmicheskie Issledovaniia, vol. 18, Nov.-Dec. 1980, p. 844-850. In Russian.

Mathematics

Kalman Filters, Optimal Control, Planetary Atmospheres, Spacecraft Control, Algorithms, Approximation, Mathematical Models, Perturbation Theory, Root-Mean-Square Errors

Scientific paper

An algorithm is examined for the state vector estimation of a spacecraft in atmospheric flight. Attention is given to the determination of an expanded state vector with allowance for a large number of heterogeneous random perturbations. A Kalman filter modification is presented which takes into account the properties of mathematical models of spacecraft motion. Recommendations on the design of a data processing unity for optimal control of a descent module in a planetary atmosphere are given.

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