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Frequenzabhängigkeit
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Response-TO-Noise Studies of Some Aircraft and Spacecraft Structures
Role of Modeling and Flight Testing in Rotorcraft Parameter Identification
Flexible Modes Control Using Sliding Mode Observers: Application to Ares I
Two Techniques for Measuring Locomotion Impact Forces during Zero G
Initial Assessment of the Ares I-X Launch Vehicle Upper Stage to Vibroacoustic Flight Environments
Fixed Base Modal Testing Using the NASA GRC Mechanical Vibration Facility
Digitalizing Existing Continuous-Data Control Systems via Continuous Frequency Matching
Human Transfer Characteristics in Flight and Ground Simulation for a Roll Tracking Task
Validation of Force Limited Vibration Testing at NASA Langley Research Center
Method for Determining the Time Delay of the Pitot-Static Tubing System of Aircraft