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- W2184597676 abstract "This paper describes the design and implementation of a Structural Load Alleviation (SLA) system for the Agusta tilt rotor/wing aircraft concept (ERICA), carried out under the European Framework V ACT-TILT project. A multi-objective controller, primarily designed to reduce the in-plane bending at the rotor blade root and the out-of plane flapping, is synthesised using an LQG (Linear Quadratic Gaussian) approach. Evaluations performed using the controller have shown that the use of cyclic control is very effective in suppressing both the build-up of in-plane loads and gimbal flapping; simultaneous suppression results in an inevitable compromise however. The issues associated with this compromise are discussed in the paper. Results from offline non-linear analysis are presented for various flight manoeuvres showing the effect of the SLA system on load suppression and manoeuvre performance." @default.
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- W2184597676 date "2005-01-01" @default.
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- W2184597676 title "Synthesis and Analysis of a Multi-Objective Controller for Tilt-Rotor Structural Load Alleviation" @default.
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