FIELD: control methods.
SUBSTANCE: disclosed is a method for controlling an air device. Air device comprises telescopic boom, strain gauges (SG) sensors for detection of bending state of telescopic boom in horizontal and vertical direction, gyroscope attached to upper part of telescopic boom, control means (50) for controlling movement of the air device based on signal values received from the SG sensors and the gyroscope. Method comprises realizing primary signals SGRaw, GYRaw from SG sensors and gyroscope. Reference signals are calculated from primary signals SGRaw, GYRaw, including SG reference signal SGRef, representing deformation value, and reference signal of gyroscope GYRef, representing angular velocity value, and angular acceleration reference signal AARef, derived from angular position or angular velocity measurement values. Restoring the first mode f1 of oscillations and second mode f2 of oscillations of higher order than first mode f1 of oscillations from reference signals and additional PAR parameters related to air device design. Values of angular compensation rate AVComp from recovered first mode f1 of oscillations and at least one second mode f2 of oscillations. Computed angular compensation rate AVComp to direct communication angular velocity value to result in drive control signal. Also disclosed is an air device. Effective damping of air device oscillations is achieved by considering connection of bending and torsion in horizontal direction.
EFFECT: method can similarly be used for damping vibrations in vertical direction, possibly including effects of hinged manipulator and cabin attached to end of hinged manipulator, for both axes.
12 cl, 8 dwg
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Authors
Dates
2019-07-18—Published
2015-12-18—Filed