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23 kwi 2007 · This chapter applies LPV techniques to the roll control of NASA Dryden’s X-53 Active Aeroelastic Wing testbed with results obtained with a set of LPV tools which makes use of object-oriented programming to enable easy construction and manipulation ofLPV models.
The X-planes are a series of experimental United States aircraft and rockets, used to test and evaluate new technologies and aerodynamic concepts. They have an X designator within the US system of aircraft designations, which denotes the experimental research mission.
17 sie 2018 · With landing gear and flaps down, NASA Dryden’s (now Armstrong’s) Active Aeroelastic Wing F/A-18A research aircraft, also known as X-53, rolled toward final approach to the Edwards Air Force Base runway at the end of a test flight in Edwards, California.
The X-53 Active Aeroelastic Wing (AAW) development program is a completed American research project that was undertaken jointly by the Air Force Research Laboratory (AFRL), Boeing Phantom Works and NASA's Dryden Flight Research Center, where the technology was flight tested on a modified McDonnell Douglas F/A-18 Hornet.
1 sty 2012 · Linear parameter-varying (LPV) techniques provide a framework for modeling, analysis, and design of the control laws across the flight envelope. This chapter applies LPV techniques to the roll control of NASA Dryden’s X-53 Active Aeroelastic Wing testbed. LPV techniques are first used to analyze a gain-scheduled classical controller.
X-53A Active Aeroelastic Wing (AAW) Test Flight. The X-53A Active Aeroelastic Wing (AAW) flight research project conducted by NASA Dryden Flight Research Center, the U.S. Air Force Research Laboratory (AFRL) and Boeing Phantom Works, researched a high-tech adaptation of the Wright Brothers rudimentary ‘wing-warping’ approach to aircraft ...
This chapter applies LPV techniques for the roll control of NASA Dryden’s X-53 Active Aeroelastic Wing testbed. LPV techniques are first used to analyze a gain-scheduled classical controller.
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