System for controlling the movement of a rotatable member

• US 4,382,216 A
• Filed: 11/30/1981
• Issued: 05/03/1983
• Est. Priority Date: 01/18/1979
• Status: Expired due to Term

• Current Assignee: FMC Corporation
• Original Assignee: FMC Corporation
• Inventors: Joseph, Craig L.
• Primary Examiner(s): Smith, Jr., David
• Application Number:
  US06/326,104
• Time in Patent Office: 519 Days
• Field of Search: 318/617, 318/618, 318/611, 318/630, 318/294, 318/327, 318/341, 318/648, 318/649, 89/41 M, 89/41 LE, 89/41 ME, 89/42 R, 74/5.4
• US Class Current: 318/630
• CPC Class Codes: F41A 27/28 Electrically-operated systems F41A27/02, F41A27/04, F41A27/30 take precedence
• CPC Class Codes: G05D 3/1463 using PID devices

Abstract

A rotatable member, such as a turret at a weapons station, is controllable about an azimuth axis. A weapon is carried in the turret with the weapon being controllable therewithin about an elevation axis. The moments of inertia of the turret and weapon about the azimuth axis and of the weapon about the elevation axis are relatively high. The disclosed system provides for elevation and azimuth control through elevation and azimuth drive trains having reflected drive train inertias which are at least two orders of magnitude smaller than the inertia of the turret and weapon about the azimuth axis and at least one order of magnitude smaller than the inertia of the weapon about the elevation axis. Further, the system senses spurious torque applied about either axis, as for example due to the recoil of the fixed weapon, and provides automatic repositioning of the controlled members about either axis to compensate for angular displacement caused by the spurious torque.

Claims

1. A system for controlling the position of a gun turret movable about an azimuth axis, wherein a rapid fire gun having a rapid fire period is mounted in the turret displaced laterally from the azimuth axis, comprising

an azimuth drive motor,

a single azimuth gear driven by said azimuth drive motor,

a ring gear meshed with said single azimuth gear and disposed so that when said drive motor is energized the turret rotates about the azimuth axis, the reflected moment of inertia of said drive motor and single azimuth gear being at least two orders of magnitude less than the turret moment of inertia about the azimuth axis,

an angular velocity sensor mounted to provide a signal indicative of the rate of turn of the turret about the azimuth axis,

a command control accessible to an operator for providing an azimuth input velocity command signal,

single means for comparing and for integrating the difference between said input command signal and said rate of turn signal and for providing an error signal responsive to said integration,

and means for coupling said error signal to said azimuth drive motor so that angular position error due to torque input about the azimuth axis caused by firing of the laterally displaced gun in the turret is corrected within the rapid fire period.

2. A system as in claim 1 wherein said means for coupling said error signal to said drive motor includes a pulse width modulator, and means for utilizing the modulated pulses to control the power supplied to said drive motor in accordance with the relative polarity of the motor drive signal so that the turret is driven in a rotational direction corresponding thereto.

3. A system as in claim 1 wherein the rapid fire gun is movable in the turret about an elevation axis and wherein the gun assembly is mounted in the turret vertically displaced from the elevation axis, together with

an elevation drive motor,

a single elevation gear driven by said elevation drive motor,

a sector gear meshed with said single elevation gear and disposed so that when said elevation drive motor is energized the gun is driven rotationally about the elevation axis, the reflected moment of inertia of said elevation drive motor and single elevation gear being at least one order of magnitude less than the gun assembly moment of inertia about the elevation axis,

an angular velocity sensor mounted to provide a signal indicative of the rate of turn of the gun about the elevation axis,

a command control accessible to the operator for providing an elevation input velocity command signal,

single means for comparing and for integrating the difference between said input command signal and said elevation rate of turn signal and for providing an error signal responsive to said elevation integration,

and means for coupling said elevation error signal to said elevation drive motor so that elevation angular position error due to torque input about the elevation axis caused by firing of the vertically displaced gun in the turret is corrected within the rapid fire period.

4. A system as in claims 1 or 3 wherein the rapid fire period is approximately 300 milliseconds.