Influence of Airframe Flexibility on Pilot-Induced Oscillations

Author:

Drewiacki Daniel1,Silvestre Flávio José1,Guimarães Neto Antônio Bernardo1

Affiliation:

1. Technological Institute of Aeronautics, 12228-900 São José dos Campos, Brazil

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Reference21 articles.

1. SmithJ. W.BerryD. T. “Analysis of Longitudinal Pilot-Induced Oscillation Tendencies of YF-12A Aircraft,” NASA TN-D-7900, Feb. 1975.

2. Prediction and Simulator Verification of Roll/Lateral Adverse Aeroservoelastic Rotorcraft–Pilot Couplings

3. YenW. Y. “Effects of Dynamic Aeroelasticity on Handling Qualities and Pilot Rating,” Purdue Univ. Rept. 77–7, Purdue, IN, Dec. 1977.

4. Design of Forcing Functions for the Identification of Human Control Behavior

5. Modeling and Simulation of Flexible Flight Vehicles

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