FIELD: control actuators of guided missiles.
SUBSTANCE: at matching of electrical and mechanical zeroes of the guided missile control actuator the potentiometer is installed in the control actuator with provision of inoperative sections at the edges of the potentiometer winding. The current collector is moved up to the stop of the controls in the extreme positions. The resistances of the inoperative sections are measured, after which the position of the current collector is shifted until the resistances of the inoperative sections get equalized with the required excess of the resistance towards the lower angle of turn of the controls, and the current collector or the kinematic transmission members are fixed.
EFFECT: enhanced accuracy and simplified operations of matching of electrical and mechanical zeroes of the control actuator with the feedback potentiometer.
4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF ESTIMATION OF GAIN FACTOR OF POTENTIOMETRIC FEEDBACK CIRCUIT OF GUIDED PROJECTILE ACTUATOR AND DEVICE FOR REALIZATION OF THIS METHOD | 2002 |
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| SELF-OSCILLATORY AUTOMATIC PILOT OF GUIDED MISSILE | 1993 |
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| GAMING DEVICE | 0 |
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| METHOD FOR CONTROL OF SPIN-STABILIZED MISSILE AND GUIDED MISSILE | 2000 |
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| AIR-DYNAMIC UNIT OF GUIDED MISSILE CONTROL ACTUATOR | 2000 |
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RU2172927C1 |
