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Simulation Study Of Impact Of Aeroelastic Characteristics On Flying Qualities Of A High Speed Civil Transport
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Book Synopsis Simulation Study of Impact of Aeroelastic Characteristics on Flying Qualities of a High Speed Civil Transport by : David L. Raney
Download or read book Simulation Study of Impact of Aeroelastic Characteristics on Flying Qualities of a High Speed Civil Transport written by David L. Raney and published by . This book was released on 2002 with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt: A piloted simulation study conducted in NASA Langley Visual Motion Simulator addressed the impact of dynamic aero- servoelastic effects on flying qualities of a High Speed Civil Transport. The intent was to determine effectiveness of measures to reduce the impact of aircraft flexibility on piloting tasks. Potential solutions examined were increasing frequency of elastic modes through structural stiffening, increasing damping of elastic modes through active control, elimination of control effector excitation of the lowest frequency elastic modes, and elimination of visual cues associated with elastic modes. Six test pilots evaluated and performed simulated maneuver tasks, encountering incidents wherein cockpit vibrations due to elastic modes fed back into the control stick through involuntary vibrations of the pilots upper body and arm.
Author :National Aeronautics and Space Adm Nasa Publisher :Independently Published ISBN 13 :9781723975578 Total Pages :94 pages Book Rating :4.9/5 (755 download)
Book Synopsis Simulation Study of Impact of Aeroelastic Characteristics on Flying Qualities of a High Speed Civil Transport by : National Aeronautics and Space Adm Nasa
Download or read book Simulation Study of Impact of Aeroelastic Characteristics on Flying Qualities of a High Speed Civil Transport written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-09-24 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt: A piloted simulation study conducted in NASA Langley Visual Motion Simulator addressed the impact of dynamic aero- servoelastic effects on flying qualities of a High Speed Civil Transport. The intent was to determine effectiveness of measures to reduce the impact of aircraft flexibility on piloting tasks. Potential solutions examined were increasing frequency of elastic modes through structural stiffening, increasing damping of elastic modes through active control, elimination of control effector excitation of the lowest frequency elastic modes, and elimination of visual cues associated with elastic modes. Six test pilots evaluated and performed simulated maneuver tasks, encountering incidents wherein cockpit vibrations due to elastic modes fed back into the control stick through involuntary vibrations of the pilots upper body and arm. Structural stiffening and compensation of the visual display were of little benefit in alleviating this impact, while increased damping and elimination of control effector excitation of the elastic modes both offered great improvements when applied in sufficient degree.Raney, David L. and Jackson, E. Bruce and Buttrill, Carey S.Langley Research CenterSUPERSONIC TRANSPORTS; FLIGHT CHARACTERISTICS; COCKPITS; STRUCTURAL VIBRATION; ACTIVE CONTROL; DYNAMIC STRUCTURAL ANALYSIS; VISUAL STIMULI; VIBRATION DAMPING; STIFFENING; PILOT PERFORMANCE; DISPLAY DEVICES; CONTROL EQUIPMENT; MOTION SIMULATORS
Book Synopsis Scientific and Technical Aerospace Reports by :
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Book Synopsis Piloted Simulation Assessment of a High-Speed Civil Transport Configuration by :
Download or read book Piloted Simulation Assessment of a High-Speed Civil Transport Configuration written by and published by . This book was released on 2002 with total page 484 pages. Available in PDF, EPUB and Kindle. Book excerpt: An assessment of a proposed configuration of a high-speed civil transport was conducted by using NASA and industry research pilots. The assessment was conducted to evaluate operational aspects of the configuration from a pilot's perspective, with the primary goal being to identify potential deficiencies in the configuration. The configuration was evaluated within and at the limits of the design operating envelope to determine the suitability of the configuration to maneuver in a typical mission as well as in emergency Or envelope-limit conditions. The Cooper-Harper rating scale was used to evaluate the flying qualities of the configuration. A summary flying qualities metric was also calculated. The assessment was performed in the Langley six-degree-of-freedom Visual Motion Simulator. The effect of a restricted cockpit field-of-view due to obstruction by the vehicle nose was not included in this study.
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Book Synopsis Monthly Catalog of United States Government Publications by :
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Book Synopsis High-speed Civil Transport Flight- and Propulsion-control Technological Issues by : J. K. Ray
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Book Synopsis Monthly Catalog of United States Government Publications by : United States. Superintendent of Documents
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Author :United States. Congress. Senate. Select Committee on Small Business Publisher : ISBN 13 : Total Pages :1442 pages Book Rating :4.:/5 (36 download)
Book Synopsis Hearings, Reports and Prints of the Senate Select Committee on Small Business by : United States. Congress. Senate. Select Committee on Small Business
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Book Synopsis Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 235) by :
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Book Synopsis Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 300) by :
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Book Synopsis International Aerospace Abstracts by :
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Author :United States. Congress. Senate. Select Committee on Small Business Publisher : ISBN 13 : Total Pages :572 pages Book Rating :4.:/5 (327 download)
Book Synopsis Technology and Management Assistance Programs of the Small Business Administration by : United States. Congress. Senate. Select Committee on Small Business
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