Real-time refinement method of spacecraft star tracker alignment estimates

• US 8,019,544 B2
• Filed: 01/03/2005
• Issued: 09/13/2011
• Est. Priority Date: 01/03/2005
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Li, Rongsheng, Needelman, David D., Wu, Yeong-Wei A.
• Primary Examiner(s): Tran; Khoi
• Assistant Examiner(s): Peche; Jorge
• Application Number:
  US11/028,094
• Publication Number:
  US 20060149474A1
• Time in Patent Office: 2,444 Days
• Field of Search: 701/207, 701/222, 701/226, 701/4, 701/13, 701/45, 701/301, 701/48, 701/70, 701/79, 701/91, 701/3, 701/224, 348/117, 280/806, 244/164, 244/171, 342/355, 180/268, 180/282
• US Class Current: 701/222
• CPC Class Codes: B64G 1/361 using star sensors
• CPC Class Codes: G01C 21/025 with the use of startrackers
• CPC Class Codes: G01S 3/7867 Star trackers navigation using star trackers G01C21/025

Abstract

A method of estimating the alignment of a star sensor (20) for a vehicle (12) includes generating star tracker data. A vehicle attitude and a star sensor attitude are determined in response to the star tracker data. A current alignment sample is generated in response to the vehicle attitude and the star sensor attitude. A current refined estimate alignment signal is generated in response to the current alignment sample and a previously refined estimate alignment signal via a vehicle on-board filter (38).

Claims

1. A method of estimating the alignment of at least one star sensor for a spacecraft, wherein said at least the star sensor resides in said vehicle comprising:

determining the alignment of said at least one star sensor with respect to an associated body of a vehicle on which the at least one star sensor resides by the steps comprising generating star tracker data from said at least one star sensor determining vehicle attitude in response to star tracker data;

determining star sensor attitude of the at least one star sensor in response to said star tracker data;

generating at least one current alignment sample of the at least one star sensor in response to said vehicle attitude and said star sensor attitude;

generating a current refined estimate alignment signal of the at least one star sensor in response to said at least one current alignment sample and a previously refined estimate alignment signal via a vehicle onboard filter.

2. A method as in claim 1 wherein said star sensor attitude is determined in response to at least one star pattern match algorithm.

3. A method as in claim 1 wherein generating at least one current alignment sample is performed recursively.

4. A method as in claim 1 wherein generating a current refined estimate alignment signal is performed recursively.

5. A method as in claim 1 wherein generating a current refined estimate alignment signal comprises generating a weighted average of said at least one current alignment sample with said previously refined estimate alignment signal.

6. A method as in claim 5 wherein generating a weighted average recursively.

7. A method as in claim 1 further comprising determining an estimated error of said current refined estimate alignment signal.

8. A method as in claim 1 wherein said at least one alignment sample comprises consecutive frames of star sensor data.

9. A method as in claim 1 wherein said at least one alignment sample comprises current attitude estimation of the at least one star sensor relative to the body of the vehicle.