초록 ▼

A stabilized sighting device for use on a carrier comprises an outer unit mounted for rotation about a bearing axis which may be parallel to the yaw axis of the carrier. An intermediate unit is mounted for rotation on the outer unit about an elevation axis and a sight unit provided with a gyro is mo

A stabilized sighting device for use on a carrier comprises an outer unit mounted for rotation about a bearing axis which may be parallel to the yaw axis of the carrier. An intermediate unit is mounted for rotation on the outer unit about an elevation axis and a sight unit provided with a gyro is mounted on the intermediate unit for rotation within a predetermined angular range about an inner axis located in a plane perpendicular to the elevation axis. First and second motors are provided for driving the intermediate unit and the sight unit about the intermediate and inner axes, respectively and are controlled by first and second servo loop circuits receiving signals from the gyroscope. A detector delivers a signal representative of the deviation of the inner unit from the canonical position and a position reproducing loop controlled by the detector actuates a motor driving the outer unit. The configuration of the outer gimbal is preferably reversed for decreasing the perturbating torques.

대표청구항 ▼

A stabilized sighting device comprising: a first gimbal unit mounted for rotation about a first axis; a drive motor for rotating said first gimbal unit about said first axis; a second gimbal unit mounted for rotation on said first gimbal unit about a second axis perpendicular to said first axis; a s

A stabilized sighting device comprising: a first gimbal unit mounted for rotation about a first axis; a drive motor for rotating said first gimbal unit about said first axis; a second gimbal unit mounted for rotation on said first gimbal unit about a second axis perpendicular to said first axis; a sight unit provided with a gyroscope and mounted on said second gimbal unit for rotation within a predetermined limited angular range with respect to a predetermined reference position which is a canonical position about a third axis perpendicular to said second axis; first and second motor means for driving said second gimbal unit and sight unit about said second and third axes, respectively; said gyroscope having a first sensitive axis located parallel to said second axis when the sight unit is in said predetermined reference position about said third axis, and a second sensitive axis parallel to said third axis, first and second servo loop circuits connected to first and second outputs of said gyroscope for controlling said first and second motor means, respectively; detector means arranged to deliver a signal representative of the deviation of said sight unit from the canonical position with respect to the second gimbal unit; and a position copying loop controlled by said detector means and activating said drive motor in a direction tending to compensate said deviation, whereby said second servo loop returns said sight unit to said predetermined reference position which is a canonical position.