Attitude displacement measurement apparatus

• US 4,706,389 A
• Filed: 08/20/1986
• Issued: 11/17/1987
• Est. Priority Date: 08/20/1986
• Status: Expired due to Fees

• Current Assignee: Karl P. Eisenhammer
• Original Assignee: Karl P. Eisenhammer
• Inventors: Eisenhammer, Karl P.
• Primary Examiner(s): Martin, Jr., William D.
• Application Number:
  US06/898,095
• Time in Patent Office: 454 Days
• Field of Search: 33/300, 33/318, 33/328, 33/324, 74/5.34, 384/461, 384/126
• US Class Current: 33/318
• CPC Class Codes: G01C 17/00 Compasses; Devices for ascertaining true or magnetic north for navigation or surveying purposes using gyroscopic effect G01C19/00
• CPC Class Codes: Y10T 74/1221 Multiple gyroscopes

Abstract

An attitude displacement measurement apparatus including a base, primary bearing means retained by the base, auxiliary bearing means mounted for rotation on the primary bearing means on a given axis with respect to the base, a first rotor mounted for rotation on the auxiliary bearing means on the given axis, a second rotor mounted for rotation on the auxiliary bearing means on the given axis, a first drive mechanism coupled to the first rotor and operable to produce rotation thereof on the auxiliary bearing means in one sense on the given axis, and a second drive mechanism coupled to the second rotor and operable to produce rotation thereof on said auxiliary bearing means on the given axis in a sense opposite to the one sense. Also included are a first sensor for sensing the rotational speed of the first rotor with respect to the base, a second sensor for sensing the rotational speed of the second rotor with respect to the base, and a comparator for determining the difference between the rotational speeds sensed by the first and second sensors.

Claims

1. Attitude displacement measurement apparatus comprising:

a base means;

primary bearing means retained by said base means;

auxiliary bearing means mounted for rotation on said primary bearing means on a given axis with respect to said base means;

a first rotor means mounted for rotation on said auxiliary bearing means on said given axis;

a second rotor means mounted for rotation on said auxiliary bearing means on said given axis;

a first drive means coupled to said first rotor means and operable to produce rotation thereof on said auxiliary bearing means in one sense on said given axis;

a second drive means coupled to said second rotor means and operable to produce rotation thereof on said auxiliary bearing means on said given axis in a sense opposite to said one sense; and

measurement means for measuring the magnitude of the difference between the relative rotational speeds of said first and second rotor means with respect to said base means.

2. An apparatus according to claim 1 wherein said first and second drive means are adapted to produce rotation of said first and second rotor means on said auxiliary bearing means at the same speed.

3. An apparatus according to claim 2 wherein said first and second drive means comprise constant speed motor means and coupling means connected between said motor means and said first and second rotor means.

4. An apparatus according to claim 3 wherein said motor means comprises a drive shaft and said coupling means comprises a first gear means coupling said drive shaft to said first rotor means and a second gear means coupling said drive shaft to said second rotor means.

5. An apparatus according to claim 4 wherein said first rotor means comprises a first rotor shaft mounted on said auxiliary bearing means in said given axis, said second rotor rotor means comprises a second rotor shaft mounted on said auxiliary bearing means and aligned with said first rotor shaft, said drive shaft is disposed perpendicular to and between said first and second rotor shafts, and said coupling means further comprises a pinion gear keyed to said drive shaft and said first and second gear means comprise a pair of gear wheels straddling and engaging said pinion gear and keyed, respectively, to said first and second rotor shafts.

6. An apparatus according to claim 5 wherein said motor means comprise a pair of constant speed motors disposed on opposite sides of said given axis, and said drive shaft comprises aligned drive shafts, one for each of said motors and connected together by said pinion gear.

7. An apparatus according to claim 6 including motor mount means supporting said first and second motors and fixed for common rotation with said auxiliary bearing means.

8. An apparatus according to claim 7 wherein said first and second rotor means are shaped and arranged to exhibit different levels of aerodynamic drag so as to produce rotation of said motor mount means in response to rotation of said first and second rotor means.

9. An apparatus according to claim 8 wherein said first rotor means comprises a first propeller with a given pitch, and said second rotor means comprises a second propeller with a pitch different than said given pitch.

10. An apparatus according to claim 9 including power supply means and slip ring means connecting said power supply means to said motor means.

11. An apparatus according to claim 10 wherein said first sensor means comprises a first optical sensor providing a first radiant energy beam periodically interrupted by said first propeller, and said second sensor means comprises a second optical sensor providing a second radiant energy beam periodically interrupted by said second propeller.

12. An apparatus according to claim 11 wherein said first optical sensor provides a first digital output signal dependent on the rotational speed of said first propeller, and said second optical sensor provides a second digital output signal dependent on the rotational speed of said second propeller.

13. An apparatus according to claim 12 wherein said comparator comprises a first digital to analog converter receiving said first output signal and producing a first analog signal, a second digital to analog converter receiving said second output signal and producing a second analog signal, and a differential amplifier receiving said first and second analog signals.

14. An apparatus according to claim 1 wherein said first and second drive means comprise motor means coupled to said first and second rotor means, and including motor mount means supporting said motor means and fixed for common rotation with said auxiliary bearing means.

15. An apparatus according to claim 14 wherein said first and second rotor means are shaped and arranged to exhibit different levels of aerodynamic drag so as to produce rotation of said motor mount means in response to rotation of said first and second rotor means.

16. An apparatus according to claim 15 wherein said motor means comprises a drive shaft and said coupling means comprises a first gear means coupling said drive shaft to said first rotor means and a second gear means coupling said drive shaft to said second rotor means.

17. An apparatus according to claim 16 wherein said first rotor means comprises a first rotor shaft mounted on said auxiliary bearing means in said given axis, said second rotor means comprises a second rotor shaft mounted on said auxiliary bearing means and aligned with said first rotor shaft, said drive shaft is disposed perpendicular to and between said first and second rotor shafts, and said coupling means further comprises a pinion gear keyed to said drive shaft and said first and second gear means comprises a pair of gear wheels straddling and engaging said pinion gear and keyed, respectively, to said first and second rotor shafts.

18. An apparatus according to claim 1 wherein said first sensor means comprises a first optical sensor providing a first radiant energy beam periodically interrupted by said first rotor means, and said second sensor means comprises a second optical sensor providing a second radiant energy beam periodically interrupted by said second rotor means.

19. An apparatus according to claim 18 wherein said first optical sensor provides a first digital output signal dependent on the rotational speed of said first propeller, and said second optical sensor provides a second digital output signal dependent on the rotational speed of said second propeller.

20. An apparatus according to claim 19 wherein said comparator comprises a first digital to analog converter receiving said first output signal and producing a first analog signal, a second digital to analog converter receiving said second output signal and producing a second analog signal, and a differential amplifier receiving said first and second analog signals.

21. An apparatus according to claim 1 wherein said measurement means comprises a first sensor means for sensing the rotational speed of said first rotor means with respect to said base means;

a second sensor means for sensing the rotational speed of said second rotor means with respect to said base means; and

comparator means for determining the difference between the rotational speeds sensed by said first and second sensor means.