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Precision Coordinate Transformation and Gravity Acceleration Algorithms

정밀좌표변환 및 중력가속도 계산 알고리듬 분석

  • 김정래 (한국항공대학교 항공우주 및 기계공학부) ;
  • 노정호 (한국항공대학교 항공우주 및 기계공학부)
  • Received : 2011.12.07
  • Accepted : 2011.12.19
  • Published : 2011.12.31

Abstract

Inertial navigation systems requires gravity model to compute gravity acceleration and its trajectory accuracy depends on the gravity model accuracy especially for a long range flight. The gravity model accuracy is important for satellite orbit prediction as well. The precision gravity model requires a precision coordinate transformation between inertial and Earth fixed coordinates. Precision gravity acceleration algorithms with a coordinate transform are studied and a computer program is developed. The effects of individual model components on trajectory error are analyzed.

Keywords

References

  1. Vallado, Fundamentals of astrodynamics and applications, 2nd ed., Microcosm, 2001.
  2. Leick, A., GPS Satellite Surveying, 3rd Edition. Willey, 2003.
  3. Hofmann-Wellenhof, et al., Global Positioning System- Theory and Practice, 5th revised edition. Springer Wien New York, 2001.
  4. International Earth Rotation and Reference Systems Service web site - http:// www.iers.org.
  5. Vetter, J.R. Nerem,R.S., Cefola,P.J. and Hagar,H., "A Historical Survey of Earth Gravitational Models Used in Astrodynamics from Sputnik and TRANSIT to GPS and TOPEX", Advances in the Astronautical Sciences, Vol. 85 , 1993, pp.1253-1273.
  6. Tapley, B., et al, "The GGM03 Mean Earth Gravity Model from GRACE", American Geophysical Union, Fall Meeting, San Francisco, California, USA, December 10-14, 2007.
  7. UTOPIA description, University of Texas at Austin, Center for Space Research, 1980.