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X-48B Flight Research Progress OverviewProgram Objectives; I. Assess stability & control characteristics of a BWB class vehicle in free-flight conditions: a) Assess dynamic interaction of control surfaces; b) Assess control requirements to accommodate asymmetric thrust; c) Assess stability and controllability about each axis at a range of flight conditions II. Assess flight control algorithms designed to provide desired flight characteristics: a) Assess control surface allocation and blending; b) Assess edge of envelope protection schemes; c) Assess takeoff and landing characteristics; d) Test experimental control laws and control design methods. III. Evaluate prediction and test methods for BWB class vehicles: a) Correlate flight measurements with ground-based predictions and measurements.
Document ID
20090005167
Acquisition Source
Armstrong Flight Research Center
Document Type
Conference Paper
Authors
Risch, Tim
(NASA Dryden Flight Research Center Edwards, CA, United States)
Cosentino, Gary
(NASA Dryden Flight Research Center Edwards, CA, United States)
Regan, Chris
(NASA Dryden Flight Research Center Edwards, CA, United States)
Kisska, Michael
(Boeing Phantom Works Huntington Beach, CA, United States)
Princen, Norman
(Boeing Phantom Works Huntington Beach, CA, United States)
Date Acquired
August 24, 2013
Publication Date
January 5, 2009
Subject Category
Aerodynamics
Meeting Information
Meeting: 47th AIAA Aerospace Sciences Meeting
Location: Orlando, FL.
Country: United States
Start Date: January 5, 2009
End Date: January 8, 2009
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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