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G-III Precision Autopilot Development in Support of UAVSAR ProgramThe primary objective of the UAVSAR Project is to develop a miniaturized polarimetric L-band synthetic aperture radar (SAR) for use on an unmanned aerial vehicle (UAV) or minimally piloted vehicle. This viewgraph presentation reviews NASA Dryden's role in the UAVSAR program. The G-III aircraft is described and shown, as well as a high level system architecture. The goals of the Platform Precision Autopilot (PPA) that it are shall fly the G-III within a 10 m (32.8 ft) diameter tube for at least 90% of each data take in conditions of calm to light atmospheric disturbances, as defined in MIL-STD-1797. That it minimize motion during data collection. It is critical to operate the UAVSAR System on a steady platform.
Document ID
20070024446
Acquisition Source
Armstrong Flight Research Center
Document Type
Conference Paper
Authors
Lee, James
(NASA Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
August 23, 2013
Publication Date
May 8, 2007
Subject Category
Aircraft Stability And Control
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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