Flight tests have been performed with a variable pitch-rate-command/attitude-hold flight control system in a Beechoraft Queen air-80 aircraft. Some results of in-flight measured runs for two pilots controlling typical easy and difficult dynamics are presented together with the initial results of the same tracking experiment performed on a ground-based flight simulator. Results are compared with results of other investigators using fixed-base flight simulators.
In-flight measured human pilot describing function and remnant for pitch attitude control
1973-01-01
Conference paper
No indication
English
Human describing functions measured in flight and on simulators
Engineering Index Backfile | 1967
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