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X-48B Flight Research - Test Progress and Instrumentation Needs for the FutureProgram 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; and 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; and 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
20090020686
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
May 12, 2009
Subject Category
Aircraft Stability And Control
Report/Patent Number
DFRC-993
Report Number: DFRC-993
Meeting Information
Meeting: International Test and Evaluation Association (ITEA) 2009 Test Instrumentation Workshop
Location: Ridgecrest, CA
Country: United States
Start Date: May 12, 2009
End Date: May 14, 2009
Distribution Limits
Public
Copyright
Public Use Permitted.
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