Method and apparatus for rotational rate determination using a stellar reference

• US 5,223,702 A
• Filed: 05/18/1992
• Issued: 06/29/1993
• Est. Priority Date: 05/18/1992
• Status: Expired due to Fees

• Current Assignee: Hughes Electronics Corporation (AT&T, Inc.)
• Original Assignee: Hughes Aircraft Company (Rtx Corporation)
• Inventors: Conley, Peter L.
• Primary Examiner(s): Nelms, David C.
• Assistant Examiner(s): LE, QUE TAN
• Application Number:
  US07/884,824
• Time in Patent Office: 407 Days
• Field of Search: 250/203.6, 250/216, 250/203.5, 250/578, 356/141, 356/152, 244/164, 244/181, 244/182, 244/176, 244/3.16, 244/3.18, 244/3.21
• US Class Current: 250/203.6
• CPC Class Codes: B64G 1/24 Guiding or controlling apparatus, e.g. for attitude control
• CPC Class Codes: B64G 1/36 using sensors, e.g. sun-sensors, horizon sensors
• CPC Class Codes: G01S 3/7867 Star trackers navigation using star trackers G01C21/025

Abstract

A method and apparatus for determining the rate of rotation of a rotating satellite 10 utilizing an imaging device 12 located on the satellite. The imaging device takes a first celestial sphere image view 22 at a first point in time and takes a second celestial image view 26 at a second point in time. The difference between the first and second images 30, differentiated over the time between the taking of the first and second images, is used to determine the rate of rotation of the satellite 32.

Claims

1. A system for determining the rate of rotation of a rotating satellite, said system comprising:

imaging means, located on the satellite, for recording first and second images of a celestial sphere, at first and second points in time, respectively; and

processing means, associated with said imaging means, for determining a relative movement of the satellite between said first and second points in time by determining a difference between said first and second images.

2. The system of claim 1 wherein said processing means includes:

storage means for storing said first recorded image until said second image has been recorded; and

logic means for determining a difference between said stored first recorded image and said second recorded image and dividing said determined difference by the time between said first and second points in time to determine a relative movement of the satellite.

3. The system of claim 2 wherein said imaging means includes means for focusing views of the celestial sphere, wherein said imaging means records first and second focused view images at said first and second respective points in time.

4. The system of claim 3 wherein said imaging means includes a detector array element adapted to detect varying levels of light intensity and wherein said first and second recorded images are represented as arrays of discrete data representative of said detected varying light intensity.

5. The system of claim 1 wherein said imaging means includes means for focusing views of the celestial sphere, wherein said imaging means records first and second focused view images at said first and second respective points in time.

6. The system of claim 5 further comprising storage means, associated with said imaging means and said processing means, for storing said first recorded image, wherein said processing means determines the difference between said stored first recorded image and said second recorded image.

7. The system of claim 6 wherein said imaging means includes a detector array element adapted to detect varying levels of light intensity and wherein said first and second recorded images are represented as arrays of discrete data representative of said detected varying light intensity.

8. A method for determining the rate of rotation of a rotating satellite, said method including:

focusing a first celestial sphere view onto an imaging device located on the satellite at a first period of time,

recording an image of the first celestial sphere on the image device;

focusing a second celestial sphere view onto said imaging device at a second period of time,

recording an image of the second celestial sphere on the image device; and

comparing said second and first recorded images to determine a relative movement of the satellite between said first and second periods of time.

9. The method of claim 8 wherein the satellite rotates about a first axis and wherein a second and third axis are perpendicular with respect to said first axis and with respect to each other, and wherein said comparison of said first and second celestial sphere images comprises:

determining a first axis relative movement component between said first and second periods of time;

determining a second axis relative movement component between said first and second periods of time; and

determining a third axis relative movement component between said first and second periods of time.

10. The method of claim 8 further including storing said first cesestial sphere image in a temporary storage device and comparing said stored first celestial sphere image to said second celestial sphere image to determine said relative movement of the satellite between said first and second periods of time.

11. The method of claim 8 wherein said imaging device comprises a detector array and a lens assembly for focusing said first and second celestial sphere views onto said detector array.

12. The method of claim 11 wherein said detector array detects varying levels of light intensity and wherein said detector array records said first and second celestial sphere views as an array of discrete data representative of said detected varying light intensity.

13. A method for determining the relative rotation of a rotating satellite over a period in time, said method including:

recording a first celestial sphere image at the beginning of the period in time;

recording a second celestial sphere image at the end of the period in time; and

determining the relative rotation over the period in time by determining the difference between said first and second recorded images.

14. The method of claim 13 further including focusing views of a celestial sphere onto an imaging device, wherein said first and second recorded celestial sphere images are recordings of a first and a second focused celestial sphere view.

15. The method of claim 13 further including storing said first recorded celestial sphere image, wherein said determined relative rotation is the difference between said stored first recorded image and said second recorded image.

16. The method of claim 14 wherein said imaging device comprises a detector array adapted to detect varying levels of light intensity and wherein a lens assembly focuses said first and second celestial sphere images onto said detector array.

17. The method of claim 16 wherein said first and second recorded celestial sphere images are recorded by said detector array as an array of discrete data representative of said detected varying light intensity.