Physics
Scientific paper
Sep 1986
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1986kosis..24..680k&link_type=abstract
Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 24, Sept.-Oct. 1986, p. 680-694. In Russian.
Physics
Aerodynamic Characteristics, Ballistic Trajectories, Iterative Solution, Parameter Identification, Spacecraft Motion, Trajectory Measurement, Algorithms, Gauss Equation, Instrument Errors, Newton Theory
Scientific paper
The proposed method is based on a combination of the successive approximation method and the continuation method. The method is applied to the nonlinear identification of the aerodynamic coefficients and initial motion conditions of a spacecraft according to measurements of its three-dimensional motion. It is shown that the proposed synthesis method is more accurate in solving this identification problem than the successive approximation method alone.
Gukov V. V.
Kostrov Alexander V.
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