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An Integrated Vehicle Modeling EnvironmentThis paper describes an Integrated Vehicle Modeling Environment for estimating aircraft geometric, inertial, and aerodynamic characteristics, and for interfacing with a high fidelity, workstation based flight simulation architecture. The goals in developing this environment are to aid in the design of next generation intelligent fight control technologies, conduct research in advanced vehicle interface concepts for autonomous and semi-autonomous applications, and provide a value-added capability to the conceptual design and aircraft synthesis process. Results are presented for three aircraft by comparing estimates generated by the Integrated Vehicle Modeling Environment with known characteristics of each vehicle under consideration. The three aircraft are a modified F-15 with moveable canards attached to the airframe, a mid-sized, twin-engine commercial transport concept, and a small, single-engine, uninhabited aerial vehicle. Estimated physical properties and dynamic characteristics are correlated with those known for each aircraft over a large portion of the flight envelope of interest. These results represent the completion of a critical step toward meeting the stated goals for developing this modeling environment.
Document ID
20020073854
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Totah, Joseph J.
(NASA Ames Research Center Moffett Field, CA United States)
Kinney, David J.
(NASA Ames Research Center Moffett Field, CA United States)
Kaneshige, John T.
(NASA Ames Research Center Moffett Field, CA United States)
Agabon, Shane
(Foothill-De Anza Community Coll. Los Altos Hills, CA, United States)
Date Acquired
August 20, 2013
Publication Date
August 9, 1999
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA Paper 99-4106
Report Number: AIAA Paper 99-4106
Meeting Information
Meeting: AIAA Atmospheric Flight Mechanics Conference
Location: Portland, OR
Country: United States
Start Date: August 9, 1999
End Date: August 11, 1999
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
PROJECT: RTOP 519-30-12
Distribution Limits
Public
Copyright
Public Use Permitted.
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