Wrapping dynamic analysis and optimization of deployable composite triangular rollable and collapsible booms

Yang, Hui; Lian, Liu; Guo, Hongwei; Lu, Fengshuai; Liu, Yongbin

doi:10.1007/s00158-018-2118-9

Cited by 32 publications

(12 citation statements)

References 21 publications

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“…The S4R element only takes into account the linear part of the nodal incremental displacement, thus significantly saving the calculation time [23]. In addition, this element type has also been successfully used in the large deformation analysis of thin-walled deployable structures [15,[21][22][23][24]. The selected element size can ensure the accuracy and efficiency of the calculation results.…”

Section: Finite Element Modelmentioning

confidence: 99%

“…The possible engineering application of DCBs for solar sails, gossamer sail systems, etc., have also been explored. Yang et al [22][23][24] established a finite element model for analyzing the coiling deformation of DCBs with triangular sections, C sections, and M sections. The structural optimization design of DCBs based on a surrogate model has also been carried out.…”

Section: Introductionmentioning

confidence: 99%

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Simplified Analytical Model for Predicting Neutral Cross-Section Position of Lenticular Deployable Composite Boom in Tensile Deformation

2021

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Foldable and deployable flexible composite thin-walled structures have the characteristics of light weight, excellent mechanical properties and large deformation ability, which means they have good application prospects in the aerospace field. In this paper, a simplified theoretical model for predicting the position of the neutral section of a lenticular deployable composite boom (DCB) in tensile deformation is proposed. The three-dimensional lenticular DCB is simplified as a two-dimensional spring system and a rigid rod, distributed in parallel along the length direction. The position of the neutral cross-section can be determined by solving the balance equations and geometric relations. In order to verify the validity of the theoretical model, a finite element model of the tensile deformation of a lenticular DCB was established. The theoretical prediction results were compared with the finite element calculation results, and the two results were in good agreement.

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Section: Finite Element Modelmentioning

confidence: 99%

Section: Introductionmentioning

confidence: 99%

Simplified Analytical Model for Predicting Neutral Cross-Section Position of Lenticular Deployable Composite Boom in Tensile Deformation

2021

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“…Non-dominated sorting genetic algorithm II is applied to realize the optimal design with a population size of 50 and generation number of 48. The value of the objective function T is equal to the sum of the objective components (O j ) with a corresponding weight factor (W j ) and scale factor (S j ) of the j-th objective component [26], i.e.,…”

Section: Multi-objective Optimization Designmentioning

confidence: 99%

Design of a New N-Shape Composite Ultra-Thin Deployable Boom in the Post-Buckling Range Using Response Surface Method and Optimization

Yang

Guo

et al. 2019

IEEE Access

Self Cite

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Composite ultra-thin boom can be folded elastically. Moreover, such booms are able to self-deploy by releasing stored strain energy, which can be applied in deployable antenna, solar sail, and optical telescopes. Surrogate models for imperfection-sensitive quantities of interest and multi-objective optimization are developed for the design of a new N-shape cross-section composite ultra-thin deployable boom. The proposed optimal design method integrates four general steps: (1) design of experiments, wherein the sampling designs of the N boom are created on the basis of the two-factor five-level full factorial design of experiments method; (2) efficient computational analyses of each design sample, wherein the post-buckling behavior of the N boom are analyzed under three different axial directions using nonlinear finite element ABAQUS/Explicit solver; (3) establishing the surrogate models of bending stiffness around the x-and y-axes and torsional stiffness around the z-axis by response surface method (RSM); (4) performing the multi-objective optimization design using modified non-dominated sorting genetic algorithm to realize the optimal design. The bending stiffness around the x-and y-axes and the torsional stiffness around the z-axis are set as the objectives, mass is set as the constraint, and the bonded web height and the central angle of the middle tape spring of the N boom are set as the variables. The typical surrogate modeling method can be applied to different problems in structural and material design.

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“…However, ultra-low frequency vibration (≤0.01 Hz) often occurs due to the randomness of environmental vibrations, which generally have a large vibration amplitude [18,19]. When the vibration amplitude is larger than the designed control stroke of the maglev vibration isolation system, a collision between the base and the floating platform occurs.…”

Section: Introductionmentioning

confidence: 99%

Tracking Control of a Maglev Vibration Isolation System Based on a High-Precision Relative Position and Attitude Model

Liu

Cui

et al. 2019

Sensors

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The maglev vibration isolation system exhibits excellent micro-vibration isolation performance (0.01 Hz to 100 Hz band) in the space environment. However, a collision between the base and the floating platform may occur in an ultra-low frequency range (≤0.01 Hz). To avoid collision, the relative position and attitude between the base and the floating platform needs to be accurately tracked and controlled. In this study, a novel measurement method with four groups of two-dimensional position-sensitive detectors equipped with four laser light sources was proposed. A high-precision relative position and attitude measurement model was established based on the geometric relationship of space coordinates. A proportional-differential (PD) fixed-point control algorithm was adopted to realize tracking control. The control performance of the system was evaluated through simulation. Experiments were also carried out to verify the stability of the system and the precision of the control algorithm. A maglev vibration isolation system prototype was constructed and a test system was established. The proposed relative position and attitude measurement model was verified and the six degrees of freedom relative position and attitude response of the system was tested. Based on the measurement model, the tracking control of the system was proven to have high precision.

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Wrapping dynamic analysis and optimization of deployable composite triangular rollable and collapsible booms

Cited by 32 publications

References 21 publications

Simplified Analytical Model for Predicting Neutral Cross-Section Position of Lenticular Deployable Composite Boom in Tensile Deformation

Simplified Analytical Model for Predicting Neutral Cross-Section Position of Lenticular Deployable Composite Boom in Tensile Deformation

Design of a New N-Shape Composite Ultra-Thin Deployable Boom in the Post-Buckling Range Using Response Surface Method and Optimization

Tracking Control of a Maglev Vibration Isolation System Based on a High-Precision Relative Position and Attitude Model

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