FIELD: automatic control of spatial maneuvering of aircraft at bounded thrust of power plant.
SUBSTANCE: proposed method is used for control of flying speed V(t) and angle of inclination of trajectory θ(t)in accordance with algorithm synthesizing deviation of throttle quadrant handle δthr.q. and normal overload ny (t) with limitations in thrust and motion parameters taken into account during operation of all aircraft control members operating in synchronism. In case of deficiency of thrust in performing the maneuver required for maintenance of the preset flying speed or in case of excessive thrust, angle of inclination of trajectory shall be corrected depending on condition of functioning of speed control circuit; speed control circuit has priority over distribution of total thrust.
EFFECT: enhanced safety of flight at automatic trajectory control of aircraft.
1 dwg
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