| Document Date: 2013-01-11 16:15:36
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City Toronto / Ithaca / Spline / / Company Astronautics Inc. / / Facility Cornell University / Upson Hall / American Institute of Aeronautics / / IndustryTerm satellite orbital states / satellite motion / carrier phase / carrier phase measurements / estimation algorithms / satellite dynamics / particular satellite / light travel time / receiver satellite / satellite constellation application / orbit solution / satellite data / candidate satellite constellation / satellite-specific parameters / satellite drag / individual satellite / beat carrier phase measurement / Adjacent satellite pairs / satellite clock error / reasonable interpolation algorithm / adjacent satellite / typical discrete-time estimation algorithm / satellite orbit determination / carrier phase version / satellite orbits / nonlinear systems / satellite constellation / interpolation algorithm / spline algorithms / satellite altitudes / satellite trajectories / estimation algorithm / scalar product / actual satellite orbit eccentricities / satellite orbit data / satellite altitude range / satellite missions / satellite-carried sensors / / Organization American Institute of Aeronautics / Sibley School of Mechanical and Aerospace Engineering / Cornell University / / Person Joanna C. Hinks / Mark L. Psiaki / / Position Professor / NRLMSISE00 model / during average solar and geomagnetic conditions / model / representative / additive noise representative / / ProvinceOrState New York / / Technology radiation / spline algorithms / reasonable interpolation algorithm / GPS / interpolation algorithm / estimation algorithms / estimation algorithm / /
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AIAA[removed]AIAA Guidance, Navigation, and Control Conference[removed]August 2010, Toronto, Ontario Canada Simultaneous Orbit and Atmospheric Density Estimation for