Identification of Programmed Contro and Intensity of Perturbations for a Flying Vehicle

Vadim Rodnishev, Kirill Denisov

Necessary conditions to identify parameters and control
of nonlinear variable stochastic systems being used to describe the operation of a flying vehicle and its subsystems are analyzed, the system parameters, control function, and states vector being bounded. The break moments as well as break points characteristics are related to a set of parameters being identified.

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