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Robot control / Control theory / Avionics / Kalman filter / Error analysis for the Global Positioning System / Global Positioning System / GPS signals / State observer / Estimation theory / Technology / GPS / Navigation


Demonstration of Adaptive Extended Kalman Filter for Low Earth Orbit Formation Estimation Using CDGPS Franz D. Busse, Stanford University Jonathan P. How, MIT James Simpson, NASA Goddard Space Flight Center INTRODUCTION
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Document Date: 2011-06-05 16:48:16

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File Size: 374,87 KB

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Portland / /

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Carrier / Naval Research Laboratory / Lear / HP / MIT Lincoln Laboratory / /

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GBP / cent / /

Facility

West Virginia University / MIT Lincoln Laboratory / University of Toronto / Stanford University / University of Maryland / Goddard Space Flight Center / Institute of Navigation GPS Meeting / /

Organization

SM / University of Maryland / MIT / Stanford University / US Federal Reserve / West Virginia University / European Space Agency / National Aeronautics and Space Administration / NASA Goddard Space Flight Center / Department of Defense / University of Toronto / Goddard Space Flight Center / /

Person

James Simpson / Franz D. Busse / Jonathan P. How / /

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Position

GNC system engineer / designer / forward / engineer / Associate Professor / /

Product

Pentax K-x Digital Camera / /

ProgrammingLanguage

MATLAB / R / C / T / /

ProvinceOrState

Maryland / /

Region

West Virginia / /

SportsLeague

Stanford University / /

Technology

GPS / ESA / simulation / using MMLE algorithms / /

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