Reaction sphere for stabilization and control in three axes

Patent metadata

Field	Value
Publication number	US-9475592-B2
Application number	US-201414170104-A
Country	US
Kind code	B2
Filing date	Jan 31, 2014
Priority date	Jan 31, 2013
Publication date	Oct 25, 2016
Grant date	Oct 25, 2016

Abstract

A system and method for controlling and stabilizing a satellite or other vehicle about any axis is disclosed. Embodiments achieve this three-axis control and stabilization with a spherical motor system or reaction sphere capable of storing momentum in a rotor. The spherical motor system comprises a spherical rotor having permanent magnets arranged in evenly-spaced antipodal pairs. Each of the permanent magnets are oriented with the same magnetic pole facing outward from a center of the rotor. The spherical motor system also comprises a stator which has magnetic sensors surrounding electromagnets. The spherical motor system further comprises a control system that controls timing and duration of energization of the electromagnets based on the detection of one of the permanent magnets by the magnetic sensors. Such a spherical motor system provides three-axis stabilization and control of a satellite (or other vehicle).

First claim

The invention claimed is:

1. A spherical motor system for control and stabilization of a vehicle in three orthogonal axes, the system comprising:
a spherical rotor having permanent magnets positioned in evenly-spaced antipodal pairs, wherein each of the permanent magnets are oriented with the same magnetic pole facing outward from a center of the rotor;
a stator having electromagnets positioned in evenly-spaced antipodal pairs that spatially correspond with the permanent magnets, the stator further having magnetic sensors surrounding at least one of each electromagnet antipodal pair to detect one of the permanent magnets; and
a control system that controls timing and duration of energization of the electromagnets based on the detection of the one of the permanent magnets with the sensors to provide the electromagnets with the opposite magnetic pole of the permanent magnets in order to attract the permanent magnets whereby momentum is transferred between the rotor and the stator along a controlled vector.

2. The spherical motor system of claim 1 , wherein the sensors are positioned along the stator such that they detect the permanent magnets only on one hemisphere of the rotor at any time.

3. The spherical motor system of claim 1 , wherein the rotor comprises non-magnetic material between the permanent magnets.

4. The spherical motor system of claim 3 , wherein the non-magnetic material is selected from the group consisting of plastic, aluminum, 300-series stainless steel, tungsten, and combinations thereof.

5. The spherical motor system of claim 1 , wherein the at least one electromagnet is centrally positioned within a ring of the sensors.

6. The spherical motor system of claim 1 , wherein the sensors are hall effect sensors.

7. The spherical motor system of claim 1 , wherein the stator includes a hollow spherical shell surrounding the rotor.

8. The spherical motor system of claim 7 , wherein the hollow spherical shell comprises a diamagnetic material.

9. The spherical motor system of claim 1 , wherein the vehicle is a satellite, and wherein the stator is connected to the satellite.

10. A method for controlling and stabilizing a vehicle in three orthogonal axes, the method comprising:
positioning permanent magnets along a spherical rotor in evenly-spaced antipodal pairs, wherein each of the permanent magnets are oriented with the same magnetic pole facing outward from a center of the rotor;
positioning electromagnets along a stator in evenly-spaced antipodal pairs that spatially correspond with the permanent magnets;
positioning magnetic sensors along the stator that surround at least one of each electromagnet antipodal pair:
detecting one of the permanent magnets with the sensors; and
controlling, with a control system, timing and duration of energization of the electromagnets based on the detecting of the one of the permanent magnets with the sensors to provide the electromagnets with the opposite magnetic pole of the permanent magnets in order to attract the permanent magnets whereby momentum is transferred between the rotor and the stator along a controlled vector.

11. The method of claim 10 , wherein the sensors are positioned along the stator such that they detect the permanent magnets only on one hemisphere of the rotor at any time.

12. The spherical motor system of claim 10 , wherein the rotor comprises non-magnetic material between the permanent magnets.

13. The method of claim 12 , wherein the non-magnetic material is selected from the group consisting of plastic, aluminum, 300-series stainless steel, tungsten, and combinations thereof.

14. The method of claim 11 , wherein the at least one electromagnet is centrally positioned within a ring of the sensors.

15. The method of claim 10 , wherein the sensors are hall effect sensors.

16. The method of claim 10 , wherein the stator includes a hollow spherical shell surrounding the rotor.

17. The method of claim 16 , wherein the hollow spherical shell comprises a diamagnetic material.

18. The method of claim 10 , wherein the vehicle is a satellite, and wherein the stator is connected to the satellite.

Assignees

• Northrop Grumman Systems Corp

Inventors

• Stagmer Emory

Classifications

• G05D1/0883

  Physics · mapped topic

• H02K11/215

  Magnetic effect devices, e.g. Hall-effect or magneto-resistive elements · CPC title

• H02K41/031

  of the permanent magnet type · CPC title

• B64G1/28 Primary

  using inertia or gyro effect · CPC title

• H02K2201/18

  Machines moving with multiple degrees of freedom · CPC title