System for vehicle attitude and/or momentum control

• US 7,273,196 B2
• Filed: 11/03/2004
• Issued: 09/25/2007
• Est. Priority Date: 11/03/2004
• Status: Expired due to Fees

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Jacobs, Jack H.
• Primary Examiner(s): DINH, TIEN QUANG
• Application Number:
  US10/980,929
• Publication Number:
  US 20060091261A1
• Time in Patent Office: 1,056 Days
• Field of Search: 244/165, 244/171, 244/164, 310/32, 310/244, 310/40.R, 74/53.4
• US Class Current: 244/165
• CPC Class Codes: B64G 1/283 using reaction wheels
• CPC Class Codes: B64G 1/286 using control momentum gyroscopes (CMGs)
• CPC Class Codes: B64G 1/425 Power storage
• CPC Class Codes: B64G 1/426 Flywheels
• CPC Class Codes: B64G 1/428 Power distribution and management
• CPC Class Codes: H02K 7/02 Additional mass for increasing inertia, e.g. flywheels
• CPC Class Codes: Y02E 60/16 Mechanical energy storage, e.g. flywheels or pressurised fluids

Abstract

A vehicle control system is provided that includes a slat having an axis, a plurality of microwheels disposed on the slat, each microwheel having a first stator wafer, a second stator wafer, and a rotor wafer disposed therebetween, the first and second stator wafers configured to spin the rotor wafer, and an actuator coupled to the slat and configured to at least partially rotate the slat about the axis.

Claims

1. A vehicle control system, comprising:

a slat having a longitudinal axis, a first edge, and a second edge;

a plurality of microwheels disposed on the slat, each microwheel having a first stator wafer, a second stator wafer, and a rotor wafer disposed therebetween, the first and second stator wafers configured to spin the rotor wafer; and

an actuator configured to at least partially rotate the slat about the longitudinal axis, the actuator including a first portion coupled to the slat first edge, a second portion coupled to the slat second edge, a cord, and an actuating mechanism, the cord coupled to the first and second edges and the actuating mechanism.

2. The vehicle control system of claim 1, wherein the first and second stator wafers each have an inner surface that defines a cavity and the rotor wafer is disposed within the cavities.

3. The vehicle control system of claim 1, wherein the first and second stator wafers are configured to magnetically levitate and spin the rotor wafer.

4. The vehicle control system of claim 1, wherein the first and second stator wafers are configured to electromagnetically levitate and spin the rotor wafer.

5. The vehicle control system of claim 1, wherein the first and second stator wafers each have electrical circuitry embedded therein.

6. The vehicle control system of claim 5, wherein each stator wafer includes an electromagnetic coil coupled thereto and each electromagnetic coil is in communication with the electrical circuitry.

7. The vehicle control system of claim 6, wherein the first and second stator wafers each include a magnet and the magnet of the first stator wafer and the magnet of the second stator wafer are configured to have opposite magnetic polarities.

8. The vehicle control system of claim 5, wherein the slat has electrical connections and the slat electrical connections are coupled to the first and second stator wafer electrical circuitry.

9. The vehicle control system of claim 1, wherein the rotor wafer has a first side and a second side, the rotor is disposed between the stator wafers such that the first side is adjacent a bottom of the first stator and the second side is adjacent a top of the second stator, wherein the first stator has a first magnetic polarity, the second stator has a second magnetic polarity, the rotor first side has a magnetic polarity opposite from the first magnetic polarity and the rotor second side has a magnetic polarity opposite from the second magnetic polarity.

10. The vehicle control system of claim 9, wherein the rotor wafer further comprises a silicon disk and a first and second magnets, the first and second magnets coupled to the rotor wafer first and second sides, respectively.

11. The vehicle control system of claim 1 wherein the stator wafers are configured to electrostatically levitate and spin the rotor wafer.

12. The vehicle control system of claim 1, wherein each microwheel is configured to spin in the same direction.

13. The vehicle control system of claim 1, wherein:

the actuator further comprises a rod and an actuating mechanism, the rod coupled to the actuating mechanism and one of the first and second edges.

14. The vehicle control system of claim 1, further comprising a first wall and a second wall, wherein the slat is disposed therebetween.

15. The vehicle control system of clam 14, wherein the actuator is disposed between the first and second wall.

16. A spacecraft control system comprising:

a plurality of slats each having a longitudinal axis, a first edge, and a second edge;

a plurality of microwheels disposed on the slat, each microwheel having a first stator wafer, a second stator wafer, and a rotor wafer disposed therebetween, the first and second stator wafers configured to levitate and spin the rotor wafer; and

an actuator coupled to the plurality of slats and configured to rotate each of the slats about its longitudinal axis, the actuator including a first portion coupled to the first edge of each slat, a second portion coupled to the second edge of each slat, a cord, and an actuating mechanism, the cord coupled to the first and second edges and the actuating mechanism.

17. The vehicle control system of claim 16, wherein:

the actuator further comprises a rod and an actuating mechanism, the rod coupled to the actuating mechanism and one of the first and second edges.

18. The vehicle control system of claim 16, further comprising a first wall and a second wall, wherein the plurality of slats is disposed therebetween.

19. The vehicle control system of clam 18, wherein the actuator is disposed between the first and second wall.

20. A vehicle, comprising:

a housing;

a plurality of slats disposed within the housing, each slat including a longitudinal axis, a first edge, and a second edge;

a plurality of microwheels disposed on each of the slats, each microwheel having a first stator wafer, a second stator wafer, and a rotor wafer disposed therebetween, the first and second stator wafers configured to spin the rotor wafer; and

an actuator including a first portion coupled to the first edge of each slat, a second portion coupled to the second edge of each slat, a cord, and an actuating mechanism, the cord coupled to the first and second edges and the actuating mechanism.

21. The vehicle of claim 20, wherein:

the actuator further comprises a rod and an actuating mechanism, the rod coupled to the actuating mechanism and one of the first and second edges.

22. The vehicle of claim 20, further comprising a first wall and a second wall, wherein the plurality of slats is disposed therebetween.

24. The vehicle of claim 22, wherein the first wall is coupled to the housing.

23. The vehicle of clam 22, wherein the actuator is disposed between the first and second wall.