Design and dynamic analysis of alpha solar rotary mechanism for China Space Station

Abstract

Purpose

The purpose of this study is to describe the proposed alpha solar rotary mechanism (ASRM) and how it is used to accurately modify the solar array of the China Space Station (CSS) in orbit to maintain continuous tracking of the sun to provide power. It also highlights the need to evaluate the performance of the ASRM and predict potential failure modes in various extreme scenarios.

Design/methodology/approach

To evaluate the performance of the ASRM, a dynamic model was created and tested under normal and faulty conditions. In addition, a multidirectional stiffness test was conducted on the prototype to verify the accuracy of the ASRM's dynamic model. The high-precision ASRM model was then used to predict potential failure modes and damaged parts in various extreme scenarios.

Findings

The simulation results were in good agreement with the test results, with a maximum error of less than 8.85%. The high-precision ASRM's model was able to accurately predict potential failure modes and damaged parts in extreme scenarios, demonstrating the effectiveness of the proposed model and simulation evaluation test.

Originality/value

The proposed high-precision ASRM model and simulation evaluation test provide an effective way to evaluate the structural safety and optimize the design of the spacecraft. This information can be used to improve the performance and reliability of the CSS's solar array and ensure continuous power supply to the station.

Citation

Zhu, J., Niu, C., Chen, J., Wang, C., Liu, D. and Yang, D. (2023), "Design and dynamic analysis of alpha solar rotary mechanism for China Space Station", Aircraft Engineering and Aerospace Technology, Vol. 95 No. 10, pp. 1531-1541. https://doi.org/10.1108/AEAT-02-2023-0053