1-15 of 15 Books
X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data
X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data
By Kenneth W. Iliff
QFT multi-input, multi-output design with non-diagonal, non-square compensation matrices
QFT multi-input, multi-output design with non-diagonal, non-square compensation matrices
By R. A. Hess
Computational analysis of forebody tangential slot blowing on the high alpha research vehicle
Computational analysis of forebody tangential slot blowing on the high alpha research vehicle
By Ken Gee
Differential canard deflection for generation of yawing moment on the X-31 with and without the vertical tail
Differential canard deflection for generation of yawing moment on the X-31 with and without the vertical tail
By Matthew Robert Whiting
Independent Orbiter assessment
Independent Orbiter assessment
By R. E. Wilson
A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane
A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane
By Frederick J. Lallman
Biomechanically induced and controller coupled oscillations experienced on the F-16XL aircraft during rolling maneuvers
Biomechanically induced and controller coupled oscillations experienced on the F-16XL aircraft during rolling maneuvers
By John W. Smith
Numerical analysis of tangential slot blowing on a generic chined forebody
Numerical analysis of tangential slot blowing on a generic chined forebody
By Roxana M. Agosta
Adaptive variable bias magnetic bearing control
Adaptive variable bias magnetic bearing control
By Dexter Johnson
A vehicle health monitoring system for the space shuttle reaction control system during reentry
A vehicle health monitoring system for the space shuttle reaction control system during reentry
By Anthony David Rosello
Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle
Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle
By Roger A. Lepsch
Relative control effectiveness technique with application to airplane control coordination
Relative control effectiveness technique with application to airplane control coordination
By Frederick J. Lallman
Computer mechanization of reentry equations with four degrees of freedom
Computer mechanization of reentry equations with four degrees of freedom
By Robert Milton Howe
Euler technology assessment for preliminary aircraft design
Euler technology assessment for preliminary aircraft design
By Todd R. Michal
A comprehensive C++ controller for a magnetically supported vertical rotor
A comprehensive C++ controller for a magnetically supported vertical rotor
By Carlos R. Morrison