Sidestick Control Evaluation Completed for Tilt‐Rotor Aircraft
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 November 1985
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
Publisher
:MCB UP Ltd
Copyright © 1985, MCB UP Limited