A real-time hybrid aeroelastic simulation platform for flexible wings-Reference-Cited by-同舟云学术

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A real-time hybrid aeroelastic simulation platform for flexible wings

Published:2019-12 Issue: Volume:95 Page:105513
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Su Weihua,Song Wei

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference18 articles.

1. Hybrid simulation system study of sins/cns integrated navigation;Wei;IEEE Aerosp. Electron. Syst. Mag.,2008

2. Aircraft control system validation via hardware-in-the loop simulation;Waszniowski;J. Aircr.,2011

3. Evolutionary optimization of a morphing wing with wind-tunnel hardware in the loop;Boria;AIAA J.,2009

4. Hardware-in-the-loop testing of a fuel cell aircraft powerplant;Bradley;J. Propuls. Power,2009

5. Pitch axis control for a guided projectile in a wind tunnel hardware-in-the-loop setup;Strub;J. Spacecr. Rockets,2015

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1. Impact of actuation and sensor measurement delays on stability of real-time hybrid aeroelastic simulation system;The Aeronautical Journal;2024-07-11

2. Numerical Analysis of Free Play-Induced Aeroelastic Phenomena: A Numerical Approach With Adaptive Step Size Control;International Journal of Aerospace Engineering;2024-04-29

3. Fluid-structure interaction simulation for multi-body flexible morphing structures;Chinese Journal of Aeronautics;2024-02

4. Study on the interaction between shaking table and eccentric load;Journal of Low Frequency Noise, Vibration and Active Control;2023-10-14

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