Effect of actuator nonlinearities on aeroservoelasticity
Author:
Affiliation:
1. Loughborough University, Loughborough LE11 3TU, England, United Kingdom
2. British Aerospace plc., Warton Aerodrome, Lancashire PR4 1AX, England, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.21620
Reference24 articles.
1. Aeroservoelastic Encounters
2. YF16 active-control-system/structural dynamics interaction instability
3. Interaction between control augmentation system and airframe dynamics on the YF-17
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2. Nonlinear Actuator Modeling for AeroServoElastic Systems Subject to Gust;AIAA SCITECH 2024 Forum;2024-01-04
3. Incorporation of Nonlinearities into Actuator Selection for Active Flutter Suppression;AIAA SCITECH 2022 Forum;2022-01-03
4. Aircraft Active Flutter Suppression: State of the Art and Technology Maturation Needs;Journal of Aircraft;2018-01
5. The Effect of Rate Limited Actuator Dynamics on the Adaptive Control of a Nonlinear Aeroservoelastic (ASE) System;52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference;2011-04-04
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