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Dynamics And Controls Flight Testing Of The X 29a Airplane

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Dynamics And Controls Flight Testing Of The X 29a Airplane

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Author :
language : en
Publisher:
Release Date : 1986

Dynamics And Controls Flight Testing Of The X 29a Airplane written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1986 with categories.

Flight Test Of The X 29a At High Angle Of Attack Flight Dynamics And Controls

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Author : Jeffrey E. Bauer
language : en
Publisher:
Release Date : 1995

Flight Test Of The X 29a At High Angle Of Attack Flight Dynamics And Controls written by Jeffrey E. Bauer and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1995 with Digital control systems categories.

Flight Test Of The X 29a At High Angle Of Attack

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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-07-06

Flight Test Of The X 29a At High Angle Of Attack written by National Aeronautics and Space Administration (NASA) and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-07-06 with categories.

The NASA Dryden Flight Research Center has flight tested two X-29A aircraft at low and high angles of attack. The high-angle-of-attack tests evaluate the feasibility of integrated X-29A technologies. More specific objectives focus on evaluating the high-angle-of-attack flying qualities, defining multiaxis controllability limits, and determining the maximum pitch-pointing capability. A pilot-selectable gain system allows examination of tradeoffs in airplane stability and maneuverability. Basic fighter maneuvers provide qualitative evaluation. Bank angle captures permit qualitative data analysis. This paper discusses the design goals and approach for high-angle-of-attack control laws and provides results from the envelope expansion and handling qualities testing at intermediate angles of attack. Comparisons of the flight test results to the predictions are made where appropriate. The pitch rate command structure of the longitudinal control system is shown to be a valid design for high-angle-of-attack control laws. Flight test results show that wing rock amplitude was overpredicted and aileron and rudder effectiveness were underpredicted. Flight tests show the X-29A airplane to be a good aircraft up to 40 deg angle of attack. Bauer, Jeffrey E. and Clarke, Robert and Burken, John J. Armstrong Flight Research Center...

X 29a Aircraft Structural Loads Flight Testing

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Author :
language : en
Publisher:
Release Date : 1989

X 29a Aircraft Structural Loads Flight Testing written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989 with categories.

Linearized Aerodynamic And Control Law Models Of The X 29a Airplane And Comparison With Flight Data

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Author : John T. Bosworth
language : en
Publisher:
Release Date : 1992

Linearized Aerodynamic And Control Law Models Of The X 29a Airplane And Comparison With Flight Data written by John T. Bosworth and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with categories.