The Bendix Corporation

Michael J Lanni

Bernard J O'Connor

John Calamera

William H Ficken

Howard E Schulien

Joseph P Pierry

Raymond M Bendett

Leon Krebs

Tony R Carnevale

A gyrocompass has a gimbal (18;218) rotatable about an upright axis (22;222) and a gyro (10;210) rotatably mounted in this gimbal (18;218) about an inner axis (16;216) transverse to the upright axis (22;222). The gyrocompass also includes a level sensor (30,32;230,232) supported by the gimbal (18;218) for providing a level signal signifying the tilt of the upright axis (22;222) from vertical. Also included is a controller (50) connected to the level sensor (30,32;230,232). The controller includes equipment (50) responsive to the level signal for rotating the gimbal (18;218) into an initial position (SP(1)) at which the level signal has a predetermined value. A method employing the foregoing apparatus includes the steps of rotating the gimbal (18;218) until the level sensor (30,32;230,232) indicates the inner axis (16;216) is horizontal. Another step is measuring the torque applied to the gyroscope (10;210) by the horizontal component of rotation of the earth with the spin axis (SA1;SA) of the gyroscope (10;210) rotated about the inner axis (16;216) into a horizontal position. Other steps are rotating the gimbal (18;218) 180 degrees and remeasuring the torque applied to the gyroscope (10;210) by the horizontal component of rotation of the earth with the spin axis (SA1;SA) of the gyroscope (10;210) rotated about the inner axis (16;216) into a horizontal position.

Gyroscopic apparatus

Apparatus is operable gyroscopically to determine direction and to determine north. This apparatus includes a case (34), a gimbal (20) and a central gyro (10). The gimbal (20) is rotatably mounted in the case for rotating azimuthally. The central gyro (10) has transverse to its spin axis (16), a single degree of rotational freedom. This central gyro (10) is mounted in the gimbal (20) to rotate about its spin axis (16) and shift the degree of freedom between a vertical (12) and a horizontal (18) axis. The central gyro (10) has a transducer (28) and a torquer (26). The transducer (28) can sense motion about the single degree of freedom and can provide a deflection signal signifying this motion. The torquer (26) is connected to the transducer (28) and can respond to its deflection signal for applying a torque to the central gyro (10) tending to affect motion about the single degree of freedom, when this freedom is oriented along the vertical axis (12). The apparatus may be used to determine north when the single degree of freedom is vertical. The torque required to restrain motion about this degree of freedom can be measured. Thereafter, the spin axis (16) can be rotated azimuthally by 90 degrees and the torque required to restrain motion about the degree of freedom remeasured. The north to south direction is estimated by applying the torque measured before and after the 90 degrees of azimuthal rotation to a predetermined trigonometric formula.

A dual suspension gyroscopic device includes a gyro having at least a single degree of freedom and defining an output axis, i.e., the sensitive axis of the gyroscopic device. The gyro is supported by a gimbal which in turn is supported in a case for unlimited angular displacement about the gimbal axis. The arrangement provides low torque suspension about the sensitive axis while permitting normal angular displacement about said axis and maintaining the gyro spin axis in a reference plane. A data transferring slip ring assembly is arranged with the gimbal support and the slip ring assembly and support arrangement is powered to minimize friction about the gimbal axis.

Dual suspension gyroscopic device having powered gimbal support

A sensor including means for operating the sensor in angular rate measuring and stabilization or rate integrating modes. When operating in the rate measuring mode, a loop is closed through an amplifier and torquer to null the sensor and when operating in the stabilization mode said loop is open and another loop is closed through a load to maintain the sensor at null. In the stabilization mode, the amplifier is used to apply command rate and drift correction signals to the sensor.

Sensor including means for operating the sensor in rate measuring and

A rate integrating device includes a torquer in open loop configuration for torquing the device to null and a load connected to the device in closed loop configuration for maintaining the device at null. The load loop includes electrical means whereby the maintenance of the device at null is controlled independent of its dynamic characteristics for increased accuracy and stability.

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Ridgewood, NJ, United States of America

Michael J Lanni