Algorithm for rapidly predicting the worst surface accuracy of deployable mesh reflectors-Reference-Cited by-同舟云学术

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Algorithm for rapidly predicting the worst surface accuracy of deployable mesh reflectors

Published:2021-10 Issue: Volume:98 Page:229-244
ISSN:0307-904X
Container-title:Applied Mathematical Modelling
language:en
Short-container-title:Applied Mathematical Modelling

Author:

Wu Xiaoshun,Cheng Runhui,Chan Tommy H.T.,Liu Guihai,Xia Juwei

Funder

China Scholarship Council

Jiangxi University of Science and Technology

National Natural Science Foundation of China

Natural Science Foundation of Jiangxi Province

Publisher

Elsevier BV

Subject

Applied Mathematics,Modeling and Simulation

Reference33 articles.

1. Active shape adjustment of large cable-mesh reflectors using novel fast mode;Xun;J. Aerosp. Eng.,2018

2. Numerical form-finding method for large mesh reflectors with elastic rim trusses;Yang;Acta Astronaut.,2018

3. Form-finding design of cable-mesh reflector antennas with minimal length configuration;Yang;Aerosp. Sci. Technol.,2017

4. An integrated control and structural design approach for mesh reflector deployable space antennas;Zhang;Mechatronics,2016

5. Integrated form finding method for mesh reflector antennas considering the flexible truss and hinges;Nie;Aerosp. Sci. Technol.,2019

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1. Kinematics and dynamics characteristics analysis of a double-ring truss deployable mechanism based on rectangular scissors unit;Engineering Structures;2024-05

2. Error Analysis of a Deployable Scissor-Like Mechanism with Joint Clearances;Advances in Mechanism and Machine Science;2023-11-05

3. Multiobjective Optimization Design of Truss Antenna;International Journal of Aerospace Engineering;2022-12-05

4. Optimization of the efficiency of large deployable reflectors by measuring the error around the feed;Acta Astronautica;2022-10

5. Structure design and kinematic analysis of a class of ring truss deployable mechanisms for satellite antennas based on novel basic units;Mechanism and Machine Theory;2022-08

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