Attitude determination studies for the Earth Observation System AM1 (EOS-AM1) mission

Journal of Guidance, Control, and Dynamics

Volumn 19, Issue 6, 1996, Pages 1326-1331

  Kudva, P ^a   Throckmorton, A ^b,c  

^a BOEING COMPANY   (United States)

^b LOCKHEED MARTIN   (United States)

^c AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; ERROR ANALYSIS; KALMAN FILTERING; MATHEMATICAL MODELS; MATRIX ALGEBRA; MONTE CARLO METHODS; PARAMETER ESTIMATION; SENSITIVITY ANALYSIS; SENSORS; SPACECRAFT OBSERVATORIES; TRACKING (POSITION);

ATTITUDE DETERMINATION; EARTH OBSERVATION SYSTEM (EOS); GYRO BIAS ESTIMATION; SENSOR NOISE; STAR FIELDS;

SPACE FLIGHT;

EID: 0030289225     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/3.21789     Document Type: Article

References (5)

1. Ford, T., "EOS Pointing Error Budget, Prediction & Verification Concept," Martin Marietta Astro Space, Design Note EOS-DN-SE&I-043A, Princeton, NJ, Aug. 1993.
2. Kudva, P., and Throckmorton, A., "EOS Attitude Determination and Next Generation Star Tracker Enhancements," AIAA Paper 93-1006, Feb. 1993.
3. Weir, P., "EOS Attitude Determination and Results," General Electric Astro Space, GE Design Note EOS-DN-GN&C-021, Princeton, NJ, March 1991.
4. Mookerjee, P., "EOS-AM Attitude Determination," General Electric Astro Space, GE Design Note EOS-DN-GN&C-034, Princeton, NJ, Nov. 1992.
5. Kudva, P., and Throckmorton, A., "Preliminary Star Catalog Development for the Earth Observation System AM1 (EOS-AM1) Mission," Journal of Guidance, Conrrol, and Dynamics, Vol. 19, No. 6, 1996, pp. 1332-1336.