FIELD: physics.
SUBSTANCE: manoeuvrable airplane flight performance manoeuvring limiter (PML) limiting device comprises an allowable angle of attack formation unit, a dampening signals generation unit, a PML static path generating unit, pitch angular velocity sensors, an angle of attack sensor, a signal source at the input of the steering drive, an adder connected in a certain manner.
EFFECT: ensuring required speed and re-regulation of aircraft exit processes at maximum allowable angle of attack, correction of angle of attack when controlling roll, possibility of exceeding maximum allowable angle of attack by a certain value.
5 cl, 8 dwg
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Authors
Dates
2020-04-22—Published
2019-05-20—Filed