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References

  1. Brouwer, D., “Solution of the Problem of Artificial Satellite Theory without Drag”, Astronomical Journal 64, 378—397, November 1959.

  2. Hilton, C.G. and Kuhlman, J.R., “Mathematical Models for the Space Defense Center”, Philco-Ford Publication No. U-3871, 17—28, November 1966.

  3. Hoots, F.R., “A Short, Efficient Analytical Satellite Theory”. AIAA Paper No. 80-1659, August 1980.

  4. Hoots, F.R., “Theory of the Motion of an Artificial Earth Satellite”, accepted for publication in Celestial Mechanics.

  5. Hujsak, R.S., “A Restricted Four Body Solution for Resonating Satellites with an Oblate Earth”, AIAA Paper No. 79-136, June 1979.

  6. Hujsak, R.S. and Hoots, F.R., “Deep Space Perturbations Ephemeris Generation”, Aerospace Defense Command Space Computational Center Program Documentation, DCD 8, Section 3, 82—104, September 1977.

  7. Kozai, Y., “The Motion of a Close Earth Satellite”, Astronomical Journal 64, 367—377, November 1959.

  8. Lane, M.H. and Cranford, K.H., “An Improved Analytical Drag Theory for the Artificial Satellite Problem”, AIAA Paper No. 69-925, August 1969.

  9. Lane, M.H., Fitzpatrick, P.M., and Murphy, J.J., “On the Representation of Air Density in Satellite Deceleration Equations by Power Functions with Integral Exponents”, Project Space Track Technical Report No. APGC-TDR-62-15, March 1962, Air Force Systems Command, Eglin AFB, FL.

  10. Lane, M.H. and Hoots, F.R., “General Perturbations Theories Derived from the 1965 Lane Drag Theory”, Project Space Track Report No. 2, December 1979, Aerospace Defense Command, Peterson AFB, CO.