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Control System Synthesis - PhD Class Exercise session 1 24/09/2020 1 The X-29 aircraft The X-29 aircraft has an unusual configuration, designed to enhance its maneuverability. It has a right half-plane pole at approximately p = 6rad/s and a right half-plane zero at z = 26rad/s. The non-minimum phase factor then writes: Pnmp(s) = z − s z + s s+ p s− p . What are the fundamental limitations ? 1. App