Model-Predictive Control of Flexible Aircraft Dynamics using Nonlinear Reduced-Order Models-Reference-Cited by-同舟云学术

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Model-Predictive Control of Flexible Aircraft Dynamics using Nonlinear Reduced-Order Models

Published:2016-01-01 Issue: Volume: Page:
ISSN:
Container-title:57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
language:
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Author:

Wang Yinan¹,Wynn Andrew¹,Palacios Rafael¹

Affiliation:

1. Imperial College London

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-0711

Reference17 articles.

1. Reexamined Structural Design Procedures for Very Flexible Aircraft

2. Nonlinear Model Reduction for Aeroelastic Control of Flexible Aircraft Described by Large Finite-Element Models

3. Gust Response Sensitivity Characteristics of Very Flexible Aircraft

4. Robust Gust Alleviation and Stabilization of Very Flexible Aircraft

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1. Large-Scale Solar-Powered UAV Attitude Control Using Deep Reinforcement Learning in Hardware-in-Loop Verification;Drones;2024-08-26

2. Effects of Geometric Nonlinearity on Flexible Wing Structures;Journal of Aircraft;2021-01

3. Data-driven nonlinear aeroelastic models of morphing wings for control;Proceedings of the Royal Society A: Mathematical, Physical and Engineering Sciences;2020-07

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