The determination of the rotational motion of a spacecraft using the results of measurements

Details The determination of the rotational motion of a spacecraft using the results of measurements The determination of the rotational motion of a spacecraft using the results of measurements

May 1989

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1989kosis..27..323a&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 27, May-June 1989, p. 323-332. In Russian.

Computer Science

Numerical Analysis

Astrodynamics, Atmospheric Entry, Least Squares Method, Rotating Bodies, Spacecraft Motion, Equations Of Motion, Numerical Integration, Optimization, Parameter Identification

Scientific paper

A method for determining the rotational motion of a spacecraft and its parameters using the results of measurements is proposed. The method involves the use of the first integrals of motion or slowly varying functions dependent on the measurement vector components. Results of a comparative numerical analysis of the proposed integral method and the least squares method are presented in problems of extraatmospheric and atmospheric spacecraft motion.

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