开环陀螺弹性多体动力学的递推公式

IF 2.7 1区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS
Shiyuan Jia, Yinghong Jia
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引用次数: 0

摘要

本文给出了开环陀螺弹性多体系统运动方程的一般递推公式。陀螺弹性多体系统是由陀螺弹性体组成的多体系统,而陀螺弹性体是由柔性体和一组双框架变速控制力矩陀螺仪(dgv)组成的。首先,用凯恩法推导了单个陀螺弹性体的运动方程。考虑了变刚度对柔体静力矩、模态动量系数、惯性矩、模态角动量系数和模态质量矩阵的影响。捕获了dgv与结构灵活性之间的相互作用。然后利用变换矩阵从柔性-柔性连接得到了具有不同连接方式的多体系统的递推运动关系。不同的连接方式包括柔-柔连接,柔-柔连接表示一个柔体连接到另一个柔体,柔-刚连接和刚-刚连接。通过分析多体系统的运动学和单个陀螺弹性体的动力学,得到了递推陀螺弹性体动力学。通过数值模拟,将该方法与基于Kane方法的直接公式进行比较,验证了该方法的准确性和有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A recursive formulation for open-loop gyroelastic multibody dynamics

In this paper, a general recursive formulation of equations of motion is presented for open-loop gyroelastic multibody systems. The gyroelastic multibody system is defined as a multibody system with gyroelastic bodies, whereas a gyroelastic body is composed of a flexible body with a cluster of double-gimbal variable-speed control moment gyroscopes (DGVs). First, the motion equations of a single gyroelastic body are derived using Kane’s method. The influence of DGVs on the static moments, modal momentum coefficients, moments of inertia, modal angular momentum coefficients, and modal mass matrix for a flexible body are considered. The interactions between the DGVs and the flexibilities of the structures are captured. The recursive kinematic relations for a multibody system with different connections are then obtained from a flexible–flexible connection using a transformation matrix. The different connections contain a flexible–flexible connection, which represents a flexible body connecting to another flexible body, flexible–rigid and rigid–rigid connections. The recursive gyroelastic multibody dynamics are obtained by analyzing the kinematics of a multibody system and the dynamics of a single gyroelastic body. Numerical simulations are presented to verify the accuracy and efficiency of the proposed approach by comparing it with a direct formulation based on Kane’s method.

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来源期刊
Astrodynamics
Astrodynamics Engineering-Aerospace Engineering
CiteScore
6.90
自引率
34.40%
发文量
32
期刊介绍: Astrodynamics is a peer-reviewed international journal that is co-published by Tsinghua University Press and Springer. The high-quality peer-reviewed articles of original research, comprehensive review, mission accomplishments, and technical comments in all fields of astrodynamics will be given priorities for publication. In addition, related research in astronomy and astrophysics that takes advantages of the analytical and computational methods of astrodynamics is also welcome. Astrodynamics would like to invite all of the astrodynamics specialists to submit their research articles to this new journal. Currently, the scope of the journal includes, but is not limited to:Fundamental orbital dynamicsSpacecraft trajectory optimization and space mission designOrbit determination and prediction, autonomous orbital navigationSpacecraft attitude determination, control, and dynamicsGuidance and control of spacecraft and space robotsSpacecraft constellation design and formation flyingModelling, analysis, and optimization of innovative space systemsNovel concepts for space engineering and interdisciplinary applicationsThe effort of the Editorial Board will be ensuring the journal to publish novel researches that advance the field, and will provide authors with a productive, fair, and timely review experience. It is our sincere hope that all researchers in the field of astrodynamics will eagerly access this journal, Astrodynamics, as either authors or readers, making it an illustrious journal that will shape our future space explorations and discoveries.
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