Synonyme wurden verwendet für:
Aircraft
•
Stability
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keywords:(Aircraft Stability and Control)
Rotorcraft control system design for uncertain vehicle dynamics using quantitative feedback theory
Identification of pilot-vehicle dynamics from in-flight tracking data
Investigation of control, display, and crew-loading requirements for helicopter instrument approach
Quantitative Feedback Theory (QFT) applied to the design of a rotorcraft flight control system
Evaluation of a technique for predicting longitudinal pilot-induced-oscillations
Effects of wing modification on an aircraft's aerodynamic parameters as determined from flight data
Advanced AFCS developments on the XV-15 tilt rotor research aircraft
Kinematic properties of rotary-wing and fixed-wing aircraft in steady coordinated high-g turns
Selection of some rotor parameters to reduce pitch-roll coupling of helicopter flight dynamics
New capabilities and recent research programs of the NASA/Army CH-47B variable-stability helicopter
Rotorcraft flight-propulsion control integration
Flight dynamics of rotorcraft in steep high-g turns
Design and evaluation of an integrated flight-control system concept for manual IFR VTOL operations