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Exploratory Studies In Generalized Predictive Control For Active Aeroelastic Control Of Tiltrotor Aircraft Nasa Tm2000 210552 Dec 6
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Book Synopsis EXPLORATORY STUDIES IN GENERALIZED PREDICTIVE CONTROL FOR ACTIVE AEROELASTIC CONTROL OF TILTROTOR AIRCRAFT... NASA/TM2000-210552... DEC. 6,. by :
Download or read book EXPLORATORY STUDIES IN GENERALIZED PREDICTIVE CONTROL FOR ACTIVE AEROELASTIC CONTROL OF TILTROTOR AIRCRAFT... NASA/TM2000-210552... DEC. 6,. written by and published by . This book was released on 2002 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781720520252 Total Pages :38 pages Book Rating :4.5/5 (22 download)
Book Synopsis Exploratory Studies in Generalized Predictive Control for Active Aeroelastic Control of Tiltrotor Aircraft by : National Aeronautics and Space Administration (NASA)
Download or read book Exploratory Studies in Generalized Predictive Control for Active Aeroelastic Control of Tiltrotor Aircraft written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-05-31 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Aeroelasticity Branch at NASA Langley Research Center has a long and substantive history of tiltrotor aeroelastic research. That research has included a broad range of experimental investigations in the Langley Transonic Dynamics Tunnel (TDT) using a variety of scale models and the development of essential analyses. Since 1994, the tiltrotor research program has been using a 1/5-scale, semispan aeroelastic model of the V-22 designed and built by Bell Helicopter Textron Inc. (BHTI) in 1981. That model has been refurbished to form a tiltrotor research testbed called the Wing and Rotor Aeroelastic Test System (WRATS) for use in the TDT. In collaboration with BHTI, studies under the current tiltrotor research program are focused on aeroelastic technology areas having the potential for enhancing the commercial and military viability of tiltrotor aircraft. Among the areas being addressed, considerable emphasis is being directed to the evaluation of modern adaptive multi-input multi- output (MIMO) control techniques for active stability augmentation and vibration control of tiltrotor aircraft. As part of this investigation, a predictive control technique known as Generalized Predictive Control (GPC) is being studied to assess its potential for actively controlling the swashplate of tiltrotor aircraft to enhance aeroelastic stability in both helicopter and airplane modes of flight. This paper summarizes the exploratory numerical and experimental studies that were conducted as part of that investigation.Kvaternik, Raymond G. and Juang, Jer-Nan and Bennett, Richard L.Langley Research CenterCONTROL SYSTEMS DESIGN; ACTIVE CONTROL; HELICOPTERS; AEROELASTICITY; AIRCRAFT CONTROL; MIMO (CONTROL SYSTEMS); STABILITY AUGMENTATION; V-22 AIRCRAFT; VIBRATION DAMPING
Book Synopsis Exploratory Studies in Generalized Predictive Control for Active Aeroelastic Control of Tiltrotor Aircraft by :
Download or read book Exploratory Studies in Generalized Predictive Control for Active Aeroelastic Control of Tiltrotor Aircraft written by and published by DIANE Publishing. This book was released on 2000 with total page 37 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Exploratory studies in generalized predictive control for active aeroelastic control of tiltrotor aircraft by : Raymond G. Kvaternik
Download or read book Exploratory studies in generalized predictive control for active aeroelastic control of tiltrotor aircraft written by Raymond G. Kvaternik and published by . This book was released on 2000 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis AIAA Journal by : American Institute of Aeronautics and Astronautics
Download or read book AIAA Journal written by American Institute of Aeronautics and Astronautics and published by . This book was released on 2006 with total page 1380 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis NASA Langley Scientific and Technical Information Output 2000 by :
Download or read book NASA Langley Scientific and Technical Information Output 2000 written by and published by . This book was released on 2001 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Smart Structures and Materials written by and published by . This book was released on 2004 with total page 606 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Journal of the American Helicopter Society by : American Helicopter Society
Download or read book Journal of the American Helicopter Society written by American Helicopter Society and published by . This book was released on 2002 with total page 628 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Simulator Study of Stall/post-stall Characteristics of a Fighter Airplane with Relaxed Longitudinal Static Stability by :
Download or read book Simulator Study of Stall/post-stall Characteristics of a Fighter Airplane with Relaxed Longitudinal Static Stability written by and published by . This book was released on 1979 with total page 236 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Parametric Study of the Aerodynamic Characteristics of Nose-cylinder-flare Bodies at a Mach Number of 6.0 by : George C. Ashby
Download or read book A Parametric Study of the Aerodynamic Characteristics of Nose-cylinder-flare Bodies at a Mach Number of 6.0 written by George C. Ashby and published by . This book was released on 1965 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Studies of Airframe-propulsion-system Integration for Mach 6 Cruise Vehicles by :
Download or read book Studies of Airframe-propulsion-system Integration for Mach 6 Cruise Vehicles written by and published by . This book was released on 1967 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Summary of Flight-test Results of the VZ-2 Tilt-wing Aircraft by : Robert J. Pegg
Download or read book Summary of Flight-test Results of the VZ-2 Tilt-wing Aircraft written by Robert J. Pegg and published by . This book was released on 1962 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Buckling of a Pressurized Toroidal Ring Under Uniform External Loading by : George E. Weeks
Download or read book Buckling of a Pressurized Toroidal Ring Under Uniform External Loading written by George E. Weeks and published by . This book was released on 1967 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of Engine-exhaust-airframe Interference on a Cruise Vehicle at Mach 6 by : James M. Cubbage
Download or read book Investigation of Engine-exhaust-airframe Interference on a Cruise Vehicle at Mach 6 written by James M. Cubbage and published by . This book was released on 1971 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results from an investigation of the effects of underexpanded engine exhaust flow on the aerodynamic performance and stability of a cruise airplane at Mach 6 are presented. The influence of wing reflex angle and nozzle geometry on exhaust flow interference effects was investigated on a flat-plate model. The experiments were conducted at a free-stream Reynolds number of 17.05 X 10 (to the 6 power) based on the length of the airplane model over a model angle-of-attack range of 0(degrees) to 10(degrees) and at nozzle static-pressure ratios from 1 to approximately 4.
Book Synopsis Analysis of Partly Wrinkled Membranes by : Manuel Stein
Download or read book Analysis of Partly Wrinkled Membranes written by Manuel Stein and published by . This book was released on 1961 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Theory for Inflated Thin-wall Cylindrical Beams by : W. B. Fichter
Download or read book A Theory for Inflated Thin-wall Cylindrical Beams written by W. B. Fichter and published by . This book was released on 1966 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flight-tested Investigation of Ailerons as a Source of Yaw Control on the VZ-2 Tilt-wing Aircraft by : Robert J. Pegg
Download or read book Flight-tested Investigation of Ailerons as a Source of Yaw Control on the VZ-2 Tilt-wing Aircraft written by Robert J. Pegg and published by . This book was released on 1962 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: