Ground Dynamics Model Validation by Use of Landing Flight Test

Volume 44, Number 6November 2007

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Topics

• Aerodynamics
• Aeronautics
• Aerospace Sciences
• Aircraft Operations and Technology
• Aircraft Stability and Control
• Aircrafts
• Aircrew
• Aviation
• Aviation Authorities and Organizations
• Aviation Safety
• Civil Aviation
• Commercial Aviation
• Flight Control Surfaces
• Flight Test
• Helicopters
• Rotorcrafts
• Unmanned Aerial Vehicle

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Keywords

• Flight Testing
• Helicopters
• Stability Derivatives
• Yaw Damper
• Federal Aviation Administration
• Damping Coefficient
• Friction Coefficient
• Unmanned Helicopter
• Flight Data
• Earth

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Digital

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• Published online22 May 2012