Pilot response during an aircraft bank-angle compensatory control task was measured by using an adaptive modeling technique. In the main control loop, which is the bank angle to aileron command loop, the pilot response was the same as that measured previously in single-input, single-output systems. The pilot used a rudder to aileron control coordination that canceled up to 80 percent of the vehicle yawing moment due to aileron deflection.
Pilot-model measurements of pilot responses in a lateral-directional control task
1976-12-01
Miscellaneous
No indication
English
Lateral-directional controller design using a pilot model and flight simulator experiments
Online Contents | 2008
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