Sidestick Control Evaluation Completed for Tilt‐Rotor Aircraft

Abstract

THE NASA/Army XV‐15 Tilt‐Rotor Research Aircraft, with a sidestick controller installed, has been flown successfully with the aircraft's stability control system both operative and inoperative. The 9‐day flight evaluation took place at NASA's Ames Research Center, Mountain View, Calif.

Citation

(1985), "Sidestick Control Evaluation Completed for Tilt‐Rotor Aircraft", Aircraft Engineering and Aerospace Technology, Vol. 57 No. 11, pp. 13-13. https://doi.org/10.1108/eb036187