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Load Alleviation Control using Dynamic Inversion with Direct Load Feedback
Proceedings of the Vertical Flight Society 77th Annual Forum and Technology Display, 2021Umberto Saetti +2 more
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Load Alleviation using Direct Load Feedback with Extremum Seeking Control
AIAA AVIATION 2022 Forum, 2022Mariano Scaramal, Joseph Horn
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2010
The main purpose of the Load Alleviation system on which this paper is focused is a drop in structural wing loads for improved performances, fatigue life, Operative Empty Weight reduction. The driving idea is to perform the alleviation during a quasi-steady symmetric maneuver by means of a symmetric actuation of dedicated control surfaces.
N. Paletta, Belardo, Marika, M. Pecora
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The main purpose of the Load Alleviation system on which this paper is focused is a drop in structural wing loads for improved performances, fatigue life, Operative Empty Weight reduction. The driving idea is to perform the alleviation during a quasi-steady symmetric maneuver by means of a symmetric actuation of dedicated control surfaces.
N. Paletta, Belardo, Marika, M. Pecora
openaire +2 more sources
Gust load alleviation on an aircraft wing by trailing edge Circulation Control
Journal of Fluids and Structures, 2021Ning Qin
exaly
Alleviation of Vortex-Induced Asymmetric Loads
Journal of Spacecraft and Rockets, 1980L.E. Ericsson, J.P. Reding
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Coandă-Type Flow Actuation for Load Alleviation
Journal of Aircraft, 2022Stefanie Düssler +2 more
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Improving flight control laws for load alleviation
2006This paper proposes a methodology to improve a given controller by taking into account additional H2 (H1) specifications. From a given model of the system and a givenlow-order controller, a particular augmented standard control problem, called Cross Standard Form (CSF), is built. The main property of this new standard problem is that the unique H2 (H1)
Alazard, Daniel +2 more
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