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A METHOD OF POSTERIOR ESTIMATION OF CHARACTERISTICS OF FLYING VEHICLE CONTROL SYSTEM

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The problem of estimation of a flying vehicle control system characteristics with the use of a limited number of field test is considered.  A method proposed to solve the problem is based on priority of the experimental data: the weight assigned to the limited field tests data exceeds the weight of practically unlimited aprioristic information. Analytical expressions for posterior estimations of the control system characteristics are derived.

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