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Use of the Variable Stability and Control X-14A to Determine Attitude Control Power and Damping Requirements for a Visual Hovering Task in a VTOL Airplane



Use of the Variable Stability and Control X-14A to Determine Attitude Control Power and Damping Requirements for a Visual Hovering Task in a VTOL Airplane

  • Presented at Forum 18
  • 6 pages
  • SKU # : 18_0_009_Rolls.pdf
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Use of the Variable Stability and Control X-14A to Determine Attitude Control Power and Damping Requirements for a Visual Hovering Task in a VTOL Airplane

Authors / Details: L. Stewart Rolls, and Fred J. Drinkwater, III