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

Abstract It is crucial to predict the worst surface accuracy of deployable mesh reflectors considering uncertainties at the design stage. The traditional method is computationally expensive because a form-finding process which needs many iterations is required in each Monte Carlo simulation. A quick method is adopted to rapidly compute the worst surface accuracy of deployable mesh reflectors. The sensitivity relationships between nodal coordinate deviations, cable force deviations and cable length errors are primarily derived. Instead of the time-consuming form-finding process, the derived sensitivity relationships are utilized to carry out the Monte Carlo simulations in the quick method. Ultimately, both the symmetric and asymmetric AstroMesh reflectors are numerically analyzed. The results show that the derived sensitivity relationships are effective, and the quick method can predict the worst surface accuracy as precise as the traditional method but with far less time consumption.

[1]  Jian Feng,et al.  Form-finding of deployable mesh reflectors using dynamic relaxation method , 2018, Acta Astronautica.

[2]  Alan Shu Khen Kwan,et al.  Unified classification of stability of pin-jointed bar assemblies , 2005 .

[3]  Hongjun Cao,et al.  Manufacturing error sensitivity analysis and optimal design method of cable-network antenna structures , 2016 .

[4]  K. Koohestani,et al.  Nonlinear force density method for the form-finding of minimal surface membrane structures , 2014, Commun. Nonlinear Sci. Numer. Simul..

[5]  C. L. Herstrom,et al.  Quasistatic Shape Adjustment of a 15-Meter-Diameter Space Antenna , 1989 .

[6]  Tao Zhang,et al.  Surface adjustment method for cable net structures considering measurement uncertainties , 2016 .

[7]  Jingli Du,et al.  Shape pre-adjustment of deployable mesh antennas considering space thermal loads , 2018 .

[8]  X. F. Yuan,et al.  Integral feasible prestress of cable domes , 2003 .

[9]  Jinwei Guo,et al.  Design and analysis of a truss deployable antenna mechanism based on a 3UU-3URU unit , 2019 .

[10]  M. Pagitz,et al.  Finite element based form-finding algorithm for tensegrity structures , 2009 .

[11]  Landolf Rhode-Barbarigos,et al.  Generation of planar tensegrity structures through cellular multiplication , 2018, Applied Mathematical Modelling.

[12]  S. Guest The stiffness of tensegrity structures , 2011 .

[13]  Dongwu Yang,et al.  An integrated control and structural design approach for mesh reflector deployable space antennas , 2016 .

[14]  Bernard Maurin,et al.  Numerical form-finding of geotensoid tension truss for mesh reflector , 2012 .

[15]  Ma Jun,et al.  Measuring full static displacements of cable domes based only on limited tested locations , 2020 .

[16]  Baiyan He,et al.  Integrated form finding method for mesh reflector antennas considering the flexible truss and hinges , 2019, Aerospace Science and Technology.

[18]  Tuanjie Li,et al.  Pretension design for space deployable mesh reflectors under multi-uncertainty , 2015 .

[19]  Yiqun Zhang,et al.  Form-finding design of cable-mesh reflector antennas with minimal length configuration , 2017 .

[20]  Bingen Yang,et al.  The fixed nodal position method for form finding of high-precision lightweight truss structures , 2019, International Journal of Solids and Structures.

[21]  J. Hedgepeth Influence of fabrication tolerances on the surface accuracy of large antenna structures , 1982 .

[22]  Shunan Wu,et al.  Active Shape Adjustment of Large Cable-Mesh Reflectors Using Novel Fast Model Predictive Control , 2018 .

[23]  Dexi Zhu,et al.  Determination of Target Modes for Monitoring the Stiffness of Cable Domes Considering Random Pretension Deviations , 2018 .

[24]  Shilin Dong,et al.  Numerical analysis of the pretension deviations of a novel crescent-shaped tensile canopy structural system , 2016 .

[25]  Bingen Yang,et al.  The Projecting Surface Method for improvement of surface accuracy of large deployable mesh reflectors , 2018, Acta Astronautica.