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An H∞ full information feedforward design approach for longitudinal motion pre¦lter design of a large §exible blended wing body (BWB) aircraft is presented. An existing onset is extended such that speci¦cations concerning command tracking, limited control energy, and manoeuvre load reduction can be addressed simultaneously. Therefore, the utilized design architecture is provided and manual tuning aspects are considered. In order to increase controller tuning e©ciency, an automated tuning process based on several optimization criteria is proposed. Moreover, two design methodologies for the parameter-varying design case are investigated. The obtained controller is validated on a high-order nonlinear model, indicating the high potential of the presented approach for §exible aircraft control.

An ℋ∞full information approach for the feedforward controller design of a large blended wing body flexible aircraft

An ℋ_∞full information approach for the feedforward controller design of a large blended wing body flexible aircraft