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Aerospace Instrument-Making Annotation << Back
A posteriori identification of angular motion of a multimodular space station under the telemetry measurements. |
M.V. Levskii
Processing’s data of the telemetric information received during controlled turns of the “Mir” orbital scientific complex, as well as a sheaf of the “Mir” orbital station with the “Atlantis” spaceship of the “Space Shuttle” space transport system of reusable are presented. The problem of exact identification of a motion (including a way of control) and determination of numerical values of parameters of control algorithm of station’s motion at the regime of a programmed turn has been solved for each turn. The method of trained models was used for processing. Because of processing, calculated motion around the center of mass during the turns of space station is reconstructed. The main parameters of the algorithm of control system are determined and entry conditions of a motion are specified. Full conformity of the measurements data to the motion of the “Mir” complex by a known way of the control of spacecraft turn (the patent of the Russian Federation for the invention № 2093433, priority – 22.03.94) is revealed. |
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