Anti-windup compensation of rate saturation in an experimental aircraft
作者： Oliver Brieger , Murray Kerr , Dirk Leibling , Ian Postlethwaite , Jorge Sofrony
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摘要: This paper describes the design, flight testing and accompanying analysis of two anti-windup (AW) compensators for an experimental aircraft - German Aerospace Center's (DLR) advanced technologies (ATTAS). The AW were designed to reduce deleterious effects rate-saturation aircraft's actuators on handling qualities. flight-tested assessed using resulting pilot comments, in form qualities ratings (HQR's) pilot-involved-oscillation (PIOR's), test data. These media demonstrate that improved predictability aircraft. results also provide initial understanding relationship between theory design choices controllers response piloted during periods rate saturation.
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