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Intelligent Control Approaches for UAVsThis talk will present overviews of various intelligent control technologies currently being developed and studied at the NASA Ames Research Center as applicable to Unmanned Aerial Vehicles (UAVs), Mars flyers, and to the next generation of flight controllers for manned aircraft. The approaches being examined include: (a) direct adaptive dynamic inverse controller, (b) adaptive critic-based optimal trajectory generator; (c) optimal allocation technique based on linear programming; (4) immunized maneuvering using autopilot building blocks. These approaches can utilize, but do not require, fault detection and isolation information. Piloted and unmanned simulation studies are performed to examine if the intelligent flight control techniques adequately: 1) match flying qualities of modem fly-by-wire flight controllers under nominal conditions; 2) improve performance under failure conditions when sufficient control authority is available; and 3) achieve intelligent maneuvering capabilities for unmanned vehicles. Results obtained so far will be presented and discussed.
Document ID
20030107319
Acquisition Source
Ames Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
KrisnaKumar, Kalmanje
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 21, 2013
Publication Date
May 29, 2003
Subject Category
Computer Programming And Software
Meeting Information
Meeting: French-Australian Advanced Workshop on Multidisciplinary Methods and Numerical Tools for UAV Design Applications
Location: Sydney
Country: Australia
Start Date: July 14, 2003
End Date: July 17, 2003
Funding Number(s)
PROJECT: RTOP 704-30-62
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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