Noise estimation for star tracker calibration and enhanced precision attitude determination

Proceedings of the 5th International Conference on Information Fusion, FUSION 2002

Volumn 1, Issue , 2002, Pages 235-242

  Lam, Quang ^a   Woodruff, Craig ^a   Ashton, Sanford ^a   Martin, David ^b  

^a NORTHROP GRUMMAN CORPORATION   (United States)

^b NASA GODDARD SPACE FLIGHT CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

INFORMATION FUSION;

ATTITUDE DETERMINATION; ATTITUDE ESTIMATION; HIGH SPATIAL FREQUENCY; INERTIAL REFERENCE UNITS; LOW-SPATIAL FREQUENCY; NONLINEAR LEAST SQUARE ESTIMATION; PRECISION ATTITUDE DETERMINATIONS; STAR TRACKER CALIBRATION;

STAR TRACKERS;

EID: 2642551912     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/ICIF.2002.1021156     Document Type: Conference Paper

References (4)

1. Q. Lam, R. Welch, and Y. Lee, "Performance Enhancement of the Stellar Inertial Attitude Determination System Via System Optimization Techniques," A Welch Engineering IR&D Report Prepared for Hughes Space and Communication, May 1997.
2. Q. Lam, C. Woodruff, S. Ashton, and D. Martin, "Ground-Based Software Tool Development for GOES Post-Launch Test Support," To be presented at the AIAA GN&C Conference 2002, August 2002, Monterey, CA.
3. B. Widrow and S. Stearns, Adaptive Signal Processing, Prentice Hall 1985, ISBN 0-13-004029-0
4. Boeing GOES N-Q Training Manual, December 2001.