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First Results from a Hardware-in-the-Loop Demonstration of Closed-Loop Autonomous Formation FlyingA closed-loop system for the demonstration of formation flying technologies has been developed at NASA s Goddard Space Flight Center. Making use of a GPS signal simulator with a dual radio frequency outlet, the system includes two GPS space receivers as well as a powerful onboard navigation processor dedicated to the GPS-based guidance, navigation, and control of a satellite formation in real-time. The closed-loop system allows realistic simulations of autonomous formation flying scenarios, enabling research in the fields of tracking and orbit control strategies for a wide range of applications. A sample scenario has been set up where the autonomous transition of a satellite formation from an initial along-track separation of 800 m to a final distance of 100 m has been demonstrated. As a result, a typical control accuracy of about 5 m has been achieved which proves the applicability of autonomous formation flying techniques to formations of satellites as close as 50 m.
Document ID
20030025267
Acquisition Source
Goddard Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Gill, E.
(Deutsche Forschungsanstalt fuer Luft- und Raumfahrt Wessling, Germany)
Naasz, Bo
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Ebinuma, T.
(Texas Univ. Austin, TX, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2003
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: 26th Annual AAS Guidance and Control Conference
Location: Breckenridge, CO
Country: United States
Start Date: February 5, 2003
End Date: February 9, 2003
Sponsors: American Astronomical Society, G and C Systems, Inc.
Distribution Limits
Public
Copyright
Public Use Permitted.
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