Add to ORKGDesign procedures for VTOL automatic control systems have been developed and are presented. Using li...
The use of throttle control laws to provide adequate flying qualities for flight path control in the...
Free-flight tests were conducted in the Langley full-scale tunnel to determine the stability and con...
Evaluation of six degrees of freedom motion simulator for Bell X-14A aircraft hovering characteristi...
Rapid air switching and low torque nozzle for dual reaction attitude control for jet VTOL aircraf
Direct side-force maneuvering system on deflected X-14A jet VTOL aircraft without changing bank angl
Both systems had full attitude command; the more complex system (Type 1) also had translational velo...
Simulation study of three instrument displays to assist airplane thrust managemen
Dynamic stability and control characteristics of 0.18 scale model of fan-in-wing VTOL aircraf
The purpose of the study was to develop generic design principles for obtaining attitude command res...
A digital self-adaptive flight control system was developed for flight test in the VTOL approach and...
Multivariable control theory is applied to the design of multiple input and output engine controls. ...
Simulations of V/STOL aircraft for autopilot research were introduced as examples of large scale sys...
Effects of coupling between pitch and roll control inputs on handling qualities of vtol aircraf
As part of NASA's program to develop technology for short takeoff and vertical landing (STOVL) fight...
Design procedures for VTOL automatic control systems have been developed and are presented. Using li...
The use of throttle control laws to provide adequate flying qualities for flight path control in the...
Free-flight tests were conducted in the Langley full-scale tunnel to determine the stability and con...
Evaluation of six degrees of freedom motion simulator for Bell X-14A aircraft hovering characteristi...
Rapid air switching and low torque nozzle for dual reaction attitude control for jet VTOL aircraf
Direct side-force maneuvering system on deflected X-14A jet VTOL aircraft without changing bank angl
Both systems had full attitude command; the more complex system (Type 1) also had translational velo...
Simulation study of three instrument displays to assist airplane thrust managemen
Dynamic stability and control characteristics of 0.18 scale model of fan-in-wing VTOL aircraf
The purpose of the study was to develop generic design principles for obtaining attitude command res...
A digital self-adaptive flight control system was developed for flight test in the VTOL approach and...
Multivariable control theory is applied to the design of multiple input and output engine controls. ...
Simulations of V/STOL aircraft for autopilot research were introduced as examples of large scale sys...
Effects of coupling between pitch and roll control inputs on handling qualities of vtol aircraf
As part of NASA's program to develop technology for short takeoff and vertical landing (STOVL) fight...
Design procedures for VTOL automatic control systems have been developed and are presented. Using li...
The use of throttle control laws to provide adequate flying qualities for flight path control in the...
Free-flight tests were conducted in the Langley full-scale tunnel to determine the stability and con...