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The study is conceived in two parts and aims to get some contributions to the problem of PIO aircraft susceptibility analysis. Part I, previously published in this journal, highlighted the main steps of deriving a complex model of human pilot. The current Part II of the paper considers a proper procedure of the human pilot mathematical model synthesis in order to analyze PIO II type susceptibility of a VTOL-type aircraft, related to the presence of position and rate-limited actuator. The mathematical tools are those of semi global stability theory developed in recent works.

PIO I-II tendencies. Part 2. Improving the pilot modeling