Reconfigurable flight control system
نویسنده
چکیده
The article explains the possibility of applying the system of parametric methods, structural reconfiguration control and reconfiguration of the object control objectives to prevent the transition to the current flight situation into a catastrophic one and maintain the specified level of safety. The article presents a block diagram of a control system developed reconfigurable dynamic system, and describes how it works. A mathematical model of the aircraft, taking into account the influence of the particular situation.
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