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The optimization of TRIAD

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MATERIAM SUPERABAT OPUS.2 Publius Ovidius Naso (43 BCE-17 CE) Metamorphoses Book II

Abstract

The optimized TRIAD algorithm of Bar-Itzhack and Harman, proposed in 1997 on the basis of insupportable premises, is shown to provide, nonetheless, the optimal solution of the Wahba problem to within terms on the order of the measurement variances. A careful rigorous derivation of the algorithm is presented as well as a comparison with the arguments of Bar-Itzhack and Harman. The algorithm is compared to a result of Markley’s.

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References

  1. BLACK, H. D. “A Passive System for Determining the Attitude of a Satellite,” AIAA Journal, Vol. 2, July 1964, pp. 1350–1351.

    Article  Google Scholar 

  2. SHUSTER, M. D. and OH, S. D. “Three-Axis Attitude Determination from Vector Observations,” Journal of Guidance and Control, Vol. 4, No. 1, Jan.–Feb. 1981, pp. 70–77.

    Article  MATH  Google Scholar 

  3. WAHBA, G. “Problem 65-1: A Least Squares Estimate of Spacecraft Attitude,” SIAM Review, Vol. 7, No. 3, July 1965, p. 409.

    Article  Google Scholar 

  4. FARRELL, J. L., STUELPNAGEL, J. C., WESSNER, R. H., and VELMAN, J. R. “Solution to Problem 65-1,” SIAM Review, Vol. 8, No. 3, July 1966, pp. 384–386.

    Article  Google Scholar 

  5. LERNER, G. M. “Three-Axis Attitude Determination,” in WERTZ, J. R. (ed.), Spacecraft Attitude Determination and Control, Springer, Berlin and New York, 1978, pp. 420–428.

    Google Scholar 

  6. MARKLEY, F. L. and MORTARI, M. “Quaternion Attitude Estimation Using Vector Measurements,” The Journal of the Astronautical Sciences, Vol. 48, Nos. 2 and 3, April–September 2000, pp. 359–380.

    Google Scholar 

  7. CHENG, Y. and SHUSTER, M. D. “Robustness and Accuracy of the QUEST Algorithm,” Paper AAS-07-102, 17th Space Flight Mechanics Meeting, Sedona Arizona, January 28–February 2, 2007; Proceedings: Advances in the Astronautical Sciences, Vol. 127, 2007, pp. 41–61.

    Google Scholar 

  8. CHENG, Y. and SHUSTER, M. D. “The Speed of Attitude Estimation,” Paper AAS-07-105, 17th Space Flight Mechanics Meeting, Sedona Arizona, January 28–February 2, 2007; Proceedings: Advances in the Astronautical Sciences, Vol. 127, 2007, pp. 101–116.

    Google Scholar 

  9. BAR-ITZHACK, I.Y. and HARMAN, R.R. “Optimized TRIAD Algorithm for Attitude Determination,” Journal of Guidance and Control, Vol. 20, No. 1, January–February 1997, pp. 208–211.

    Article  MATH  Google Scholar 

  10. SHUSTER, M. D. “A Survey of Attitude Representations,” The Journal of the Astronautical Sciences, Vol. 41, No. 4, October–December 1993, pp. 439–517.

    MathSciNet  Google Scholar 

  11. SHUSTER, M. D. “Constraint in Attitude Estimation Part I: Constrained Estimation,” M. D. Shuster, The Journal of the Astronautical Sciences, Vol. 51, No. 1, January–March 2003, pp. 51–74.

    MathSciNet  Google Scholar 

  12. SHUSTER, M. D. “Constraint in Attitude Estimation Part II: Unconstrained Estimation,” The Journal of the Astronautical Sciences, Vol. 51, No. 1, January–March 2003, pp. 75–101.

    MathSciNet  Google Scholar 

  13. SORENSEN, H.W. Parameter Estimation, Marcel Dekker, New York 1980.

    Google Scholar 

  14. CHENG, Y. and SHUSTER, M. D. “QUEST and the Anti-QUEST: Good and Evil Attitude Estimation,” The Journal of the Astronautical Sciences, Vol. 53, No. 3, July–September 2005, pp. 337–351.

    Google Scholar 

  15. SHUSTER, M. D. “The TRIAD Algorithm as Maximum-Likelihood Estimation,” The Journal of the Astronautical Sciences, Vol. 54, No. 1, January–March 2006, pp. 113–123.

    MathSciNet  Google Scholar 

  16. SHUSTER, M. D. “Maximum Likelihood Estimation of Spacecraft Attitude,” The Journal of the Astronautical Sciences, Vol. 37, No. 1, January–March 1989, pp. 79–88.

    Google Scholar 

  17. MORTARI, D. “EULER-2 and EULER-n Algorithms for Attitude Determination from Vector Observations,” Space Technology, Vol. 16, Nos. 5–6, 1996, pp. 317–321.

    Article  Google Scholar 

  18. MARKLEY, F. L. “Attitude Determination Using Two Vector Measurements,” Proceedings, Flight Mechanics Symposium, NASA Goddard Space Flight Center, Greenbelt, MD, May 1999, NASA Conference Publication NASA/CP-19989-209235, pp. 39–52.

    Google Scholar 

  19. Markley, F. L. “Unit Quarternion from Rotation Matrix,” submitted to the Journal of Guidance, Control and Dynamics.

  20. SHEPPERD, S.W. “Quaternion from Rotation Matrix,” Journal of Guidance and Control, Vol. 1, 1978, pp. 223–224.

    MATH  Google Scholar 

  21. MARKLEY, F. L. “Attitude Determination Using Vector Observations: a Fast Optimal Matrix Algorithm,” The Journal of the Astronautical Sciences, Vol. 41, No. 2, April–June 1993, pp. 261–280.

    MathSciNet  Google Scholar 

  22. SHUSTER, M. D. and FREESLAND, D. C. “The Statistics of TASTE and the Inflight Estimation of Sensor Precision,” Proceedings, NASA Flight Mechanics Symposium, NASA Goddard Space Flight Center, Greenbelt, Maryland, October 18–20, 2005.

    Google Scholar 

  23. BAR-ITZHACK, I.Y. and MEYER, J. “On the Convergence of Iterative Orthogonalization Processes,” IEEE Transactions on Aerospace and Electronic Systems, Vol. AES-12, March 1976, pp. 146–151.

    Google Scholar 

  24. TANYGIN, S. and SHUSTER, M. D. “The Many TRIAD Algorithms,” Paper AAS-07-104, AAS/AIAA Space Flight Mechanics, Meeting, Sedona, Arizona, January 28–February 22, 2007; Proceedings: Advances in the Astronautical Sciences, Vol. 127, 2007, pp. 81–99.

    Google Scholar 

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Correspondence to Malcolm D. Shuster.

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Shuster, M.D. The optimization of TRIAD. J of Astronaut Sci 55, 245–257 (2007). https://doi.org/10.1007/BF03256523

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