Study conducted by Northrop Corp to determine optimum shaping of control power which provides handling qualities that require little effort on part of pilot to maintain good control; two-axis moving base simulator used and test program for altitude control (throttle), roll, pit and yaw control are described; criterion used to determine optimum control was pilot's opinion based on Cooper rating system; results obtained.
Moving base simulator study of all mechanical control system for VTOL aircraft
AIAA -- Tech Papers
Simulation for Aerospace Flight Conference ; 1963 VTOL-STOL
AIAA -- Technical Papers ; p 117-123
1963
7 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
AUTOLAND SYSTEM FOR VTOL AIRCRAFT, VTOL AIRCRAFT, AND LANDING CONTROL METHOD FOR VTOL AIRCRAFT
Europäisches Patentamt | 2024
|Flying VTOL Flight Simulator Study
NTIS | 1960
|