Synonyme wurden verwendet für:
Frequenzabhängigkeit
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Accurate Prediction of Longitudinal Flying Qualities for Landing Aircraft
AMTD - Advanced Mirror Technology Development in Mechanical Stability
AMTD -Advanced Mirror Technology Development in Mechanical Stability
An Improved Ground Vibration Test Method. Volume I. Research Report
Auralization of NASA N+2 Aircraft Concepts from System Noise Predictions
Compensator Improvement with an Application to a Large Space Vehicle
Demonstration of Frequency-Sweep Testing Technique Using a Bell 214-ST Helicopter
Digitalizing Existing Continuous-Data Control Systems via Continuous Frequency Matching
Dynamic Loads Analysis of Space Vehicle Systems - Launch and Exit Phase
Electro-Mechanical Actuator. DC Resonant Link Controller
Evaluation of a Digital Flight Controller for a Flexible-Fighter Aircraft
Evaluation of Image Amplifier Components of Night, AERIAL Photographic Reconnaissance Systems
Experimental Damping Studies Monthly Progress Report, 6 Jul. - 5 Aug. 1965
Exterior Electromagnetic Response of NASA F-106 Aircraft
Fast Response Vanes for Sensing Flow Patterns in Helicopter Rotor Environment
Fixed Base Modal Testing Using the NASA GRC Mechanical Vibration Facility
Flexible Modes Control Using Sliding Mode Observers: Application to Ares I
FRATE (Freight Car Response Analysis and Test Evaluation), Volume I: User's Manual
Frequency-Domain Identification of XV-15 Tilt-Rotor Aircraft Dynamics
Generation of Two-Dimensional Gust Fields in Subsonic Wind-Tunnels
Ground Vibration Test of an F-16 Airplane with Modified Decoupler Pylons
Human Pilot Response During Single- and Multi-Axis Tracking Tasks
Human Transfer Characteristics in Flight and Ground Simulation for a Roll Tracking Task
Hybrid Propulsion for Launch Vehicle Boosters: A Program Status Update
Initial Assessment of the Ares I-X Launch Vehicle Upper Stage to Vibroacoustic Flight Environments
Integrating Flight Dynamics & Control Analysis and Simulation in Rotorcraft Conceptual Design
Limiting Performance of Nonlinear Systems with Applications to Helicopter Vibration Control Problems