Radially actuated control moment gyroscope

• US 6,834,561 B2
• Filed: 08/22/2002
• Issued: 12/28/2004
• Est. Priority Date: 08/22/2002
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Meffe, Marc E.
• Primary Examiner(s): PANG, ROGER L
• Application Number:
  US10/227,218
• Publication Number:
  US 20040035229A1
• Time in Patent Office: 859 Days
• Field of Search: 74/5.R, 74/52.2, 74/54, 74/54.1, 74/54.6, 74/54.7, 74/56.R, 74/56.D, 74/56.E
• US Class Current: 74/5.46
• CPC Class Codes: B64G 1/286 using control momentum gyroscopes (CMGs)
• CPC Class Codes: Y10T 74/125 by magnetic field
• CPC Class Codes: Y10T 74/1254 by motor torque
• CPC Class Codes: Y10T 74/1261 with pick off
• CPC Class Codes: Y10T 74/1264 Optical

Abstract

The present invention provides a control moment gyroscope that overcomes many of the limitations of the prior art. The control moment gyroscope provides a radial actuator mechanism to provide rotation to an inner gimbal assembly around a gimbal axis. The radial actuator mechanism comprises a circular ring at the midpoint of the gimbal axis, the circular ring extending around the outer periphery of the inner gimbal assembly housing. The radial actuator mechanism rotates the inner gimbal assembly around the gimbal axis through the use of a non-contact motor that provides rotational force directly to the outer perimeter of the inner gimbal assembly. Because the inner gimbal assembly is rotated from the midpoint of the gimbal axis, a torque module assembly at the end of the gimbal axis is not required. Thus, the overall length of the control moment gyroscope can be reduced. Additionally, the cost and life limiting attributes of the torque module assembly can be eliminated, and the operational bandwidth of the gyroscope increased. Finally, because the inner gimbal assembly is rotated from the outer perimeter, the torque provided to the inner gimbal assembly is naturally increased by the leverage arm of the inner gimbal assembly.

Claims

1. A control moment gyroscope comprising:

a) an inner gimbal assembly, the inner gimbal assembly including a rotor rotating on a rotor axis, the inner gimbal assembly rotateable on a gimbal axis to create a torque moment, the inner gimbal assembly including a housing surrounding the rotor and having a outer periphery perpendicular to the gimbal axis; and

b) a radial actuator mechanism, the radial actuator mechanism including;

i) a ring surrounding the outer periphery of the housing, the ring including a motor rotor;

ii) a motor stator, the motor stator and motor rotor providing a controllable rotational force at the outer periphery of the housing to controllably rotate the inner gimbal assembly

iii) a power-signal transfer device for transferring power and a control signal to the inner gimbal assembly, wherein the power-signal transfer device comprises a low frequency AC coupler and a high frequency AC coupler at least partially affixed to the ring.

2. The control moment gyroscope of claim 1 wherein the control moment gyroscope further includes a rotational position sensor.

3. The control moment gyroscope of claim 1 wherein the control moment gyroscope is affixed to a vehicle with a base ring assembly, and wherein the ring is affixed to the base ring assembly and the motor stator is affixed to the inner gimbal assembly.

4. The control moment gyroscope of claim 1 wherein the control moment gyroscope is affixed to a vehicle with a base ring assembly, and wherein the motor stator is affixed to the base ring assembly and the ring is affixed to the inner gimbal assembly.

5. The control moment gyroscope of claim 1 wherein the control moment gyroscope is affixed to a vehicle with pillow blocks, and wherein the ring is affixed to the vehicle and the motor stator is affixed to the inner gimbal assembly.

6. The control moment gyroscope of claim 1 wherein the control moment gyroscope is affixed to a vehicle with pillow blocks, and wherein the motor stator is affixed to the vehicle and the ring is affixed to the inner gimbal assembly.

7. A control moment gyroscope comprising:

a) an inner gimbal assembly, the inner gimbal assembly including a rotor rotating on a rotor axis, the inner gimbal assembly rotateable on a gimbal axis to create a torque moment, the inner gimbal assembly including a housing surrounding the rotor and having a outer periphery perpendicular to the gimbal axis; and

b) a radial actuator mechanism, the radial actuator mechanism including;

i) a ring surrounding the outer periphery of the housing, the ring including a motor rotor;

ii) a motor stator, the motor stator and motor rotor providing a controllable rotational force at the outer periphery of the housing to controllably rotate the inner gimbal assembly;

iii) power-signal transfer device for transferring power and a control signal to the inner gimbal assembly, the power signal transfer device comprising a low frequency AC coupler and a high frequency AC coupler; and

iv) a rotational position sensor, the rotational position sensor including an optical encoder pattern formed on the ring and an optical encoder pickoff.