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Embedded Relative Navigation Sensor Fusion Algorithms for Autonomous Rendezvous and Docking Missionsbd Systems (a subsidiary of SAIC) has developed a suite of embedded relative navigation sensor fusion algorithms to enable NASA autonomous rendezvous and docking (AR&D) missions. Translational and rotational Extended Kalman Filters (EKFs) were developed for integrating measurements based on the vehicles' orbital mechanics and high-fidelity sensor error models and provide a solution with increased accuracy and robustness relative to any single relative navigation sensor. The filters were tested tinough stand-alone covariance analysis, closed-loop testing with a high-fidelity multi-body orbital simulation, and hardware-in-the-loop (HWIL) testing in the Marshall Space Flight Center (MSFC) Flight Robotics Laboratory (FRL).
Document ID
20080013593
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
DeKock, Brandon K.
(bd Systems, Inc. Huntsville, AL, United States)
Betts, Kevin M.
(bd Systems, Inc. Huntsville, AL, United States)
McDuffie, James H.
(bd Systems, Inc. Huntsville, AL, United States)
Dreas, Christine B.
(bd Systems, Inc. Huntsville, AL, United States)
Date Acquired
August 24, 2013
Publication Date
January 28, 2008
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: Institute of Navigation National Technical Meeting 2008: Innovating together Exploring the Future Uses of Navigation of Technology
Location: San Diego, CA
Country: United States
Start Date: January 28, 2008
End Date: January 30, 2008
Sponsors: Institute of Navigation
Funding Number(s)
CONTRACT_GRANT: NNM06AB28C
Distribution Limits
Public
Copyright
Public Use Permitted.
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