X 29 Flight Control System

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X 29 Flight Control System Lessons Learned

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Author : Robert Clarke
language : en
Publisher:
Release Date : 1994

X 29 Flight Control System Lessons Learned written by Robert Clarke and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1994 with Aerodynamics categories.

X 29 Flight Control System

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Author :
language : en
Publisher:
Release Date : 1994

X 29 Flight Control System written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1994 with Aerodynamics categories.

X 29 Flight Research Program

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Author :
language : en
Publisher:
Release Date : 1984

X 29 Flight Research Program written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1984 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 Aerodynamics categories.

Multivariable Control Law Design For The X 29 Aircraft

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Author :
language : en
Publisher:
Release Date : 1984

Multivariable Control Law Design For The X 29 Aircraft written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1984 with categories.

Flight control laws are designed for the X-29 forward swept wing demonstrator aircraft using a design technique based on multivariable control law theory developed professor Brian Porter. The computer-aided design program called MULTI is used to develop and refine the control laws. MULTI also simulates the complete closed-loop control system and generated appropriate time response plots for analysis. Aircraft dynamics for several points in the flight envelope are represented by linearized state space equations obtained from NASA Dryden, and agency responsible for the development and testing of the X-29. Decoupled longitudinal and lateral equations are used to design separate longitudinal and lateral controllers. Control laws are developed to stabilize the aircraft and perform longitudinal maneuvers (direct climb, vertical translation, and beta pointing) at three different flight conditions, with and without first order-actuator dynamics and computational time delay added to the simulation. The responses are compared. Originator-supplied keywords include: Wings, Swept wings, Supercritical Wings, Flight control systems; Fly-by-wire control, and Airfoils.

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.

Buffet Induced Structural Flight Control System Interaction Of The X 29a Aircraft

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Author :
language : en
Publisher:
Release Date : 1991

Buffet Induced Structural Flight Control System Interaction Of The X 29a Aircraft written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1991 with categories.

Operational Viewpoint Of The X 29a Digital Flight Control System

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Author :
language : en
Publisher:
Release Date : 1988

Operational Viewpoint Of The X 29a Digital Flight Control System written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1988 with categories.

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 Control System Design Factors For Applying Automated Testing Techniques

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Author : Joel R. Sitz
language : en
Publisher:
Release Date : 1990

Flight Control System Design Factors For Applying Automated Testing Techniques written by Joel R. Sitz and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1990 with Airplanes categories.