Integrated Dynamics of Space Rigid-Flex Combination System with Time-Varying Configuration

Author:

Xie Yaen1ORCID,Zhang Xianliang2ORCID,Song Xiangshuai1ORCID,Lian Xiaobin3ORCID,Zhang Jian3

Affiliation:

1. College of Aerospace and Civil Engineering, Harbin Engineering University, Harbin 150001, China

2. School of Mathematics and Statistics, Taishan University, Taian 271021, China

3. Shanghai Institute of Satellite Engineering, Shanghai 201109, China

Abstract

Dual numbers were applied to the dynamics of a rigid-flexible combination system (RFCS) with time-varying configuration in this paper. The six-dimensional spinor form of the motion of flexible modules, including the dual vector, dual momentum, dual inertia operator, dual coupling coefficient operator, and dual-modal coordinates, was derived using the dual numbers that could represent spiral motion in a compact form. On this basis, the integrated dynamic model of a rigid-flexible combination system with a time-varying configuration was proposed. And then, the relative dynamics equations between two rigid-flexible combination systems which both have time-varying configuration were provided. An on-orbit assembly mission of flexible modules transported and operated by free-flying space robots (FFSRs) is presented as an exemplary application of relative dynamics. Simulation results illustrate the complex coupling effects on the relative motion between two rigid-flex combination systems with time-varying configuration.

Publisher

Hindawi Limited

Subject

Aerospace Engineering

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