2020
DOI: 10.1109/access.2020.2993813
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Surface Shape Stability Design of Mesh Reflector Antennas Considering Space Thermal Effects

Abstract: On-orbit periodic thermal loads degrade the reflector surface accuracy of AstroMesh antennas. To address this problem, a surface shape stability design method is proposed to passively pre-control the on-orbit thermal deformation of mesh reflectors, in which the structural parameters are properly designed to make the internal forces of the whole structure change coordinately and the surface shape of cable-mesh antennas insensitive to thermal loads. First, mathematical models of mechanical-thermal matching (MTM)… Show more

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Cited by 10 publications
(3 citation statements)
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“…A design method that only relies on the uniformity of tension to obtain thermal stability does not consider the structural deformation caused by the thermal environment, which is also related to the material properties and geometric configuration of the structure. Based on this, Yang et al [6] designed the cross-sectional area of each cable element under the constraint that the overall mass of the cable element is constant. Numerical simulations show that the surface accuracy of the cable net is not affected by temperature.…”
Section: Introductionmentioning
confidence: 99%
“…A design method that only relies on the uniformity of tension to obtain thermal stability does not consider the structural deformation caused by the thermal environment, which is also related to the material properties and geometric configuration of the structure. Based on this, Yang et al [6] designed the cross-sectional area of each cable element under the constraint that the overall mass of the cable element is constant. Numerical simulations show that the surface accuracy of the cable net is not affected by temperature.…”
Section: Introductionmentioning
confidence: 99%
“…Guo et al proposed a thermal compensation and precompensation design for an antenna and carried out a prestressed design according to the temperature load [7]. Yang et al designed a typical AstroMesh reflector structure to stabilize the surface shape and proposed a method to precontrol the in-orbit thermal deformation of the grid reflector to reduce the thermal deformation of the reflector in the entire temperature range [8]. Nie et al analysed the coupling effect of a truss and cable net in the thermal deformation process, reduced the thermal deformation error by improving the optimization model, and reduced the in-orbit profile error of the reflector by optimizing the thermal structure model [9,10].…”
Section: Introductionmentioning
confidence: 99%
“…Many scholars have proposed different optimization methods to solve this problem. Yang et al (2020) proposed to stabilize the surface shape by pre-controlling the on-orbit thermal deformation of mesh reflectors and designing a typical AstroMesh reflector structure to reduce the thermal deformation of the reflectors in the whole temperature range. Guo et al (2016) proposed the thermal compensation and pre-compensation design of the antenna, and carried out the pre-stress design according to the temperature load.…”
Section: Introductionmentioning
confidence: 99%