Deformation Analysis of the Multiplanar Conformal Off-Axis Four-Mirror in an Aerospace Environment

The effect of maneuver overload on a new type of the multiplanar conformal off-axis four-mirror is studied under the noninertial environment of aerospace. Two kinds of maneuvering flight, horizontal maneuvering and vertical maneuvering, are taken as examples, and the force analysis of the aircraft i...

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Published inInternational Journal of Aerospace Engineering Vol. 2021; pp. 1 - 10
Main Authors Huo, Haodong, Ji, Shijun, Zhao, Ji, Sun, Rengquan, Dai, Handa
Format Journal Article
LanguageEnglish
Published New York Hindawi 2021
John Wiley & Sons, Inc
Hindawi Limited
Wiley
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Abstract The effect of maneuver overload on a new type of the multiplanar conformal off-axis four-mirror is studied under the noninertial environment of aerospace. Two kinds of maneuvering flight, horizontal maneuvering and vertical maneuvering, are taken as examples, and the force analysis of the aircraft in the noninertial environment is considered. And the force analysis of the aircraft and the multiplanar conformal off-axis four-mirror is connected by the overload coefficient. Finally, the finite element simulation analysis of the multiplanar conformal off-axis four-mirror is carried out. The results show that the influence of maneuver overload on the multiplanar conformal off-axis four-mirror cannot be ignored. Large overload will result in large deformation of the multiplanar conformal off-axis four-mirror. The deformation is closely related to the structure of the multiplanar conformal off-axis four-mirror. Under the action of lateral force, nonuniform deformation is more likely to occur on the surface of the multiplanar conformal off-axis four-mirror.
AbstractList The effect of maneuver overload on a new type of the multiplanar conformal off-axis four-mirror is studied under the noninertial environment of aerospace. Two kinds of maneuvering flight, horizontal maneuvering and vertical maneuvering, are taken as examples, and the force analysis of the aircraft in the noninertial environment is considered. And the force analysis of the aircraft and the multiplanar conformal off-axis four-mirror is connected by the overload coefficient. Finally, the finite element simulation analysis of the multiplanar conformal off-axis four-mirror is carried out. The results show that the influence of maneuver overload on the multiplanar conformal off-axis four-mirror cannot be ignored. Large overload will result in large deformation of the multiplanar conformal off-axis four-mirror. The deformation is closely related to the structure of the multiplanar conformal off-axis four-mirror. Under the action of lateral force, nonuniform deformation is more likely to occur on the surface of the multiplanar conformal off-axis four-mirror.
Audience Academic
Author Huo, Haodong
Sun, Rengquan
Ji, Shijun
Zhao, Ji
Dai, Handa
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Copyright Copyright © 2021 Haodong Huo et al.
COPYRIGHT 2021 John Wiley & Sons, Inc.
Copyright © 2021 Haodong Huo et al. This is an open access article distributed under the Creative Commons Attribution License (the “License”), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License. https://creativecommons.org/licenses/by/4.0
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Snippet The effect of maneuver overload on a new type of the multiplanar conformal off-axis four-mirror is studied under the noninertial environment of aerospace. Two...
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SubjectTerms Aerospace engineering
Aerospace environments
Aircraft
Deformation
Deformation analysis
Design
Finite element analysis
Finite element method
Gravity
Horizontal flight
Interferometry
Optimization
Overloading
Parameter estimation
Power plants
Random vibration
Vertical flight
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Title Deformation Analysis of the Multiplanar Conformal Off-Axis Four-Mirror in an Aerospace Environment
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