Guilhem Puyou

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Following the works presented in St Petersburg during the 16th IFAC Symposium on Automatic Control in Aerospace, Airbus has been working on the design and evaluation of more integrated control laws, taking into account multi-objectives design criteria, gathering from the very beginning the specifications in term of handling qualities, comfort, loads, and(More)
This paper deals with the synthesis of an open-loop control law of a civilian aircraft for the compensation of the pitching moment generated by the extension of airbrakes. The proposed method uses in-flight recorded data and is based on impulse response identification and inverse simulation, whose results are used to design the controller upon qualitative(More)
This paper describes the application of an indirect LFT (Linear Fractional Transformation) -based adaptive control scheme to a rigid transport aircraft, with emphasis on the lateral axis. The plant parameters, namely the stability derivatives, are estimated online using a Recursive Least Squares technique. A modal approach is used to directly synthesize the(More)
<lb>The development process of critical avionics products are done under<lb>strict safety regulations. These regulations include determinism and<lb>predictability of the systems’ timing. The overall approach is based on a<lb>separation of concerns between control design and implementation. One<lb>of the toughest challenges in the current approach is the(More)
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