Encapsulation Based Method for Natural Frequency Identification of Deployable Solar Arrays with Multiple Plates

Chunjuan Zhao,Xiangyu Zhao,Lei Zhang,Shanbo Chen,Jisong Yu,Jiaxi Zhou

doi:10.1155/2021/7443312

Abstract

The ground modal test is an important approach to the natural frequency of solar arrays to support the attitude control of spacecraft. However, for the batch production of small satellites, the accuracy and efficiency of traditional ground modal testing methods are limited. This shortcoming restricts the development of satellite constellations. Based on the encapsulation method widely used in the computer field, this paper proposed a natural frequency identification method of deployable solar arrays with multiple plates. This method is of high accuracy and efficiency that meets the demand of attitude control and makes sense to accelerate the batch production of small satellites. First, a suspended modal test system with gravity compensation function is designed. Second, the mathematical model of the test system is established. Abstracting parts of the parameters of the test object into an encapsulated entity, the mathematical model is simplified by equivalent variables. Thus, the direct mapping relationship between the ground test result and the true natural frequency is proposed. Finally, to verify the identification accuracy, finite element analysis (FEA) and the ground modal test of a two-folder solar array simulant are carried out. The results show that the relative error of the first-order natural frequency after correction and the theoretical value is less than 3%. Meanwhile, the identification accuracy of the ground modal test is improved by more than 50%. This method improves the availability of ground test results and reduces the calculation amount, so that it is convenient for engineering applications.

Highlights

Academic Editor: Jiaxi Zhou e ground modal test is an important approach to the natural frequency of solar arrays to support the attitude control of spacecraft
Based on the encapsulation method widely used in the computer field, this paper proposed a natural frequency identification method of deployable solar arrays with multiple plates. is method is of high accuracy and efficiency that meets the demand of attitude control and makes sense to accelerate the batch production of small satellites
To verify the identification accuracy, finite element analysis (FEA) and the ground modal test of a two-folder solar array simulant are carried out. e results show that the relative error of the first-order natural frequency after correction and the theoretical value is less than 3%

Summary

Test System and Mathematical Model

Accurate measurement of modal information is important for dynamic modeling and structural optimization. N) (where keqy is the equivalent stiffness of the substructure in the vertical direction), and the simplified mathematical model of the natural circular frequency in the vertical direction under the testing state can be obtained as ωy f􏼐mj, Δmj, keqy, k􏼑. Under the ground test conditions, the first-order natural frequency of the solar array measured by the suspended modal test system in the horizontal direction is given as 1 fx 2πfx􏼐keqx􏼑. E true stiffness matrix and the test stiffness matrix of solar arrays are expressed with the equivalent stiffness E time and complexity of natural frequency identification will be reduced, and this makes sense to the batch production of small satellites

Simulation Verification

Method in this paper

S2imulation mode

Findings

Conclusion