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A Self-Tuning Kalman Filter for Autonomous Navigation Using the Global Positioning System (GPS)Most navigation systems currently operated by NASA are ground-based, and require extensive support to produce accurate results. Recently developed systems that use Kalman filter and GPS (Global Positioning Systems) data for orbit determination greatly reduce dependency on ground support, and have potential to provide significant economies for NASA spacecraft navigation. These systems, however, still rely on manual tuning from analysts. A sophisticated neuro-fuzzy component fully integrated with the flight navigation system can perform the self-tuning capability for the Kalman filter and help the navigation system recover from estimation errors in real time.
Document ID
19990046605
Acquisition Source
Goddard Space Flight Center
Document Type
Reprint (Version printed in journal)
Authors
Truong, Son H.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Date Acquired
August 19, 2013
Publication Date
January 1, 1999
Subject Category
Aircraft Communications And Navigation
Meeting Information
Meeting: Flight Mechanics
Location: Greenbelt, MD
Country: United States
Start Date: May 18, 1999
End Date: May 20, 1999
Distribution Limits
Public
Copyright
Other

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