Research concerning pilot-in-the-loop handling qualities has traditionally assumed that a pilot is focused upon maintaining a specific parameter, such as aircraft attitude or normal acceleration. This assumption has resulted in many important results and, by modeling this type of pilot behavior, a significant amount of predictive ability. In spite of these successes, many aspects of pilot control remain very difficult to predict. It is hypothesized that pilots often engage in a previously unrecognized type of tracking, boundary-avoidance tracking, where the goal is to avoid a hazardous parameter, such as ground impact, or a routine limit, such as an assigned minimum altitude. A variety of Simulink ® models were built to study this phenomenon and it was found that treating the pilot gain as a function of the time to exceeding a given boundary can result in the type of control inputs typical of pilots in such situations, including the worst types of pilot-induced oscillations.
Nomenclature
K bm= maximum boundary gain t b = time to boundary t min = minimum time to boundary with no boundary feedback t max = time to boundary when boundary feedback is the maximum boundary gain, K bm τ b = time delay for boundary-avoidance feedback x b = displacement from boundary