SYSTEM FOR ADAPTIVE CONTROL OF AEROPLANE ON PITCH ANGLE

摘要

FIELD: physics. ^ SUBSTANCE: system comprises a pitch angle selector, the control object (aeroplane), an angle sensor, an angular velocity sensor, a standard model, a parameter sensor, a parameter selector, six adders, five amplifiers, two multiplier units, two integrators and two differentiators. The second adder, integrator, multiplier unit, fourth adder, parameter sensor and parameter selector form variable-parameter filter. ^ EFFECT: improved quality of the transient process and faster operation. ^ 1 dwg