外对接机制与宇宙飞船收敛动能积累的数学模型

Andrey Vladimirovich Yaskevich
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引用次数: 0

摘要

新的外围对接机制是按照国际对接系统标准(IDSS)设计的对接单元的一部分。该机构的运动学基于Gough-Stewart平台。弹簧机构用于航天器接近动能的转换。然而,传统的阻尼被能量累积所取代。因此,设计中包含了新的器件。本文所建立的对接机构的动力学数学模型考虑了对接机构的主要特点——运动学、惯性特性和由分离装置产生的内力。该模型与航天器的运动方程和对接单元接触相互作用分析算法一起构成了用于分析从第一次接触到收放结束的运动学和动力学过程的对接数学模型的一部分。关键词:航天器,对接机构,动力学方程。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Математическая модель динамики периферийного стыковочного механизма с накоплением кинетической энергии сближения космических аппаратов
The new peripheral docking mechanism is part of a docking unit designed in compli-ance with the International Docking System Standard (IDSS). The mechanism kinematics is based on the Gough-Stewart platform. Spring mechanisms are used for transformation of spacecraft approach kinetic energy. However, traditional damping is replaced by energy ac-cumulation. Therefore, the design includes new devices. The dynamic math model of the dock-ing mechanism described in this paper takes into account its main features – kinematics, inertia properties and generation of internal active forces by separate devices. Along with spacecraft motion equations and algorithms of docking unit contact interaction analysis, this model is part of a docking math model used for the analysis of kinematics and dynamics processes from the first contact to the end of retraction. Key words: spacecraft, docking mechanism, dynamics equations.
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