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This paper describes a mathematical identification of time constants for pilot behavior during a helicopter control process. Based on this mathematical identification and a mathematical description of helicopter dynamics, a simulation scheme was built in the Simulink® environment. Subsequently, the analysis of time constant changes in a pilot behavior model during helicopter longitudinal motion was...
The paper follows previous research of a mechatronic system, in terms of the pilot action/intervention to the flight control system. In this paper authors focus on the system behavior owing to a step disturbance to the plant. The plant under consideration represents the longitudinal dynamics of an aircraft, and an associated feedback controller to augment the damping pitch. Various pilot models are...
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