Wind Tunnel Test for Videogrammetric Deformation Measurement of UAV for Mars Airplane Balloon Experiment-1 (MABE-1)

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ISSN Print: 2329-3322
ISSN Online: 2329-3330
www.scirp.org/journal/jfcmv
E-mail: jfcmv@scirp.org

"Wind Tunnel Test for Videogrammetric Deformation Measurement of UAV for Mars Airplane Balloon Experiment-1 (MABE-1)"
written by Koji Fujita, Akira Oyama, Daisuke Kubo, Masahiro Kanazaki, Hiroki Nagai,
published by Journal of Flow Control, Measurement & Visualization, Vol.7 No.2, 2019

has been cited by the following article(s):

[1]	Aeroelastic deformation measurement of Martian airplane for high-altitude flight experiment using stereophotogrammetry
	2021

[2]	ステレオ写真測量法の適用による火星探査航空機の空力弾性変形に関する研究
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[3]	Deployable Wing Model Using ANCF and UVLM: Multibody Dynamic Simulation and Wind Tunnel Experiment
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[4]	The challenge of controlling a small Mars exploration plane
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[5]	The challenge of controlling a small Mars plane
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[6]	Flexible multibody dynamics using absolute nodal coordinate formulation with internal constraint equation
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[7]	Multibody modeling using absolute nodal coordinate plate element for deployable aerospace structures
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[1]	Calculation Method for Air Data Based on UKF with Information from INS and FADS 2022 China Automation Congress (CAC), 2022 DOI:10.1109/CAC57257.2022.10056097

[2]	Aeroelastic deformation measurement of Martian airplane for high-altitude flight experiment using stereophotogrammetry Engineering Research Express, 2021 DOI:10.1088/2631-8695/abe920

[3]	Deployable Wing Model Using ANCF and UVLM: Multibody Dynamic Simulation and Wind Tunnel Experiment AIAA Scitech 2020 Forum, 2020 DOI:10.2514/6.2020-1678

[4]	Solar Planets and Exoplanets [Working Title] 2020 DOI:10.5772/intechopen.95507

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