Simulation experiments to determine the feasibility of landing V/TOL aircraft on ships at sea were studied. The motion and attitude of the aircraft relative to the landing platform was known at the instant of touchdown. The success of these experiments depended on the ability of the experimenter to measure the pilot's performance during the landing maneuver. To facilitate these measurements, the equations describing the motion of the aircraft and its attitude relative to the landing platform are presented in a form which is suitable for simulation purposes.
Measures of Pilot Performance During V/Tol Aircraft Landings on Ships at Sea
1977
23 pages
Report
Keine Angabe
Englisch
NTIS | 1972
Simulating aircraft landings in fog
Engineering Index Backfile | 1950
|PILOT CUEING FOR ROTORCRAFT SHIPBOARD LANDINGS
TIBKAT | 2020
|Pilot Cueing for Rotorcraft Shipboard Landings
AIAA | 2020
|