Welcome to Acta Armamentarii ! Today is Share:

Acta Armamentarii ›› 2023, Vol. 44 ›› Issue (5): 1513-1520.doi: 10.12382/bgxb.2022.0055

Previous Articles     Next Articles

Collaborative Proportional Method for Measuring Triaxial Moment of Inertia Based on Vibration Compound Pendulum and Torsion Pendulum

YANG Hongtao, LU Zhihui, SUN Haozhi, WU Yiyong, LIU Min, LAI Yanbo   

  1. Zhengzhou Research Institute of Mechanical Engineering Co., Ltd., Zhengzhou 450052, Henan, China
  • Received:2022-01-22 Online:2022-07-03

Abstract:

A body moving in space needs to do circular swing along three orthogonal directions respectively during the measurement of its triaxial moment of inertia. To reduce the number of azimuth adjustment, a coollaborative proportional method for measuring the triaxial moment of inertia based on vibration compound pendulum and torsion pendulum is proposed. The equipment structure is described, and the full-parameter calculation formula and approximate calculation formula of the proposed method are given. Error analysis is done to this method and a comparison is made with the torsion pendulum method. Simulators are used as the measurement object, and the proposed method is experimentally studied. The experimental results indicate that: the computational results of the two formulas are basically the same when Jz/Jy is less than 1.02; when Jz/Jy is greater than 1.02, only the full-parameter calculation formula can be used, which can also solve the problem of triaxial measurement of the moment of inertia of winged flying bodies; the proposed method and the collaborative difference method previously developed constitute the complete measurement system, which can meet the requirements of certain types of revolving body and heteromorphic body with wings for the triaxial measurement of moment of inertia.

Key words: triaxial moment of inertia, collaborative measurement, vibration compound pendulum, torsion pendulum, collaborative proportional measuring method