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Aerospace Instrument-Making

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Method for determination of optimal operational autonomous control the movement of the aircraft center of mass
Petrov I.O.

Considered a new method for determining the optimum operational autonomous control of the center of mass of the aircraft. The method is based on energy theory of synergetic maneuver that allows the structure of optimal control the movement of the center of mass of the aircraft using only phase aircraft coordinates at the current point of the trajectory. This circumstance makes managing operational and autonomous. Demonstrated that the optimal operational control should be determined for absolute motion ofaircraft, but aerodynamic forces define the vector of relative airspeed. This approach more accurately reflects the reality and improves the accuracy of traffic aircraft control. The proposed method for the determination of optimal control of motion of center of mass of the aircraft shows versatility and efficiency energy approach and its applicability to the manoeuvres of aircraft in all phases of flight in the atmosphere both inside and outside. Synergistic maneuvering at high speeds requires operational objectives to control the orientation of the aircraftbased optimal adaptive control algorithms directly on board well ahead of time to maneuver. Therefore, the author of the method based on energy theory led to the establishment of a universal operational autonomous control algorithms that implement all technical possibilities of the system of air and space. The author of the method allows you to create terminal guidance algorithms implemented in tempeaircraft flightand EGR solution accuracy target of any disturbances in the real movement ofaircraftand the online conversion management optionsin the pace of flight. The author of the new mathematical model of the motion of center of mass of aircraft and new operational method for determination of optimal programsmovement of the aircraftcenter of massallows you to solve the emerging problem of synergetic maneuvering, both theoretically and in a practical sense.
Key words: aircraft manoeuvres, prompt optimal control, energy theory, speed of change of kinetic ener-gy, power surface forces.


Contacts: E-mail: petrovigor63@mail.ru

Pp. 22-29.

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