Attitude dynamics of a spacecraft with variable structure at presence of harmonic perturbations

Anton V. Doroshin; Mikhail M. Krikunov

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Attitude dynamics of a spacecraft with variable structure at presence of harmonic perturbations

机译：具有谐波扰动的具有可变结构的航天器的姿态动力学

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摘要

Attitude dynamics of a spacecraft (SC) with variabie structure (inertia-mass parameters variation) is examined. Equations of the motion of the SC are obtained on the base of Hamiltonian formalism in Serret-Andoyer variables. These equations can be used for analysis and synthesis of conditions of the SC attitude motion on active legs of orbital trajectories. Analytical and numerical modeling of the SC motion is realized. Existence of the SC chaotic modes of motion is demonstrated with the help of Melnikov method and Poincar£ sections. Also attitude motion of a dual-spin spacecraft (DSSC) is considered at presence of small internal harmonic torque between DSSC coaxial bodies.

机译：研究了具有可变结构（惯性质量参数变化）的航天器（SC）的姿态动力学。 SC的运动方程是在Serret-Andoyer变量的汉密尔顿形式主义的基础上获得的。这些方程式可用于分析和合成轨道轨迹的活动腿上的SC姿态运动的条件。实现了SC运动的解析和数值建模。借助梅尔尼科夫方法和庞加莱截面证明了SC混沌运动的存在。此外，在DSSC同轴物体之间存在小的内部谐波转矩的情况下，还考虑了双旋航天器（DSSC）的姿态运动。

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来源
《Applied Mathematical Modelling》 |2014年第8期|2073-2089|共17页
作者
Anton V. Doroshin; Mikhail M. Krikunov;
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作者单位

Space Engineering Department (Division of Flight Dynamics and Control Systems), Samara State Aerospace University (National Research University),Moskovskoe shosse 34, Samara 443086, Russian Federation;

Space Engineering Department (Division of Flight Dynamics and Control Systems), Samara State Aerospace University (National Research University),Moskovskoe shosse 34, Samara 443086, Russian Federation;

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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
中图分类
关键词
Spacecraft; Dual-spin spacecraft; Variable structure; Hamiltonian; Phase portrait; Serret-Andoyer variables;

机译：航天器;双旋飞船;可变结构;哈密顿相像;Serret-Andoyer变量;

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1. Attitude Dynamics and Tracking Control of Spacecraft in the Presence of Gravity Oblateness Perturbations [J] . Achim IONITA, Ionel POPESCU INCAS Bulletin . 2016,第1期

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2. Robust dynamic output feedback control for attitude stabilization of spacecraft with nonlinear perturbations [J] . Liu Chuang, Sun Zhaowei, Shi Keke, Aerospace science and technology . 2017,第MAY期

机译：具有非线性扰动的航天器姿态稳定的动态输出反馈鲁棒控制
3. The theory of canonical perturbations applied to attitude dynamics and to the Earth rotation. Osculating and nonosculating Andoyer variables [J] . Michael Efroimsky, Alberto Escapa Celestial Mechanics and Dynamical Astronomy: An international journal of space dynamics . 2007,第4期

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4. Adaptive Neural Network Control of Spacecraft Rendezvous using Nonlinear Dynamical Models in the presence of J_2 perturbations [C] . Kewen Zhang, Michael A. Demetriou AIAA guidance, navigation, and control conference;AIAA SciTech forum . 2018

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5. Dynamics of a variable mass system applied to spacecraft rocket attitude theory. [D] . Mudge, Jason Dominic. 1999

机译：应用于航天器火箭姿态理论的变质量系统动力学。
6. Finite-Time Attitude Stabilization Adaptive Control for Spacecraft with Actuator Dynamics [O] . Chunbao Wang, Dong Ye, Zhongcheng Mu, 2019

机译：具有执行器动力学的航天器航天器的有限时间态度稳定控制
7. The theory of canonical perturbations applied to attitude dynamics and to the Earth rotation. Osculating and nonosculating Andoyer variables [O] . Efroimsky, Michael, Escapa, Alberto 2007

机译：规范扰动理论应用于态度动力学和动力学到地球自转。密切和非拟合的andoyer变量
8. Theory of Canonical Perturbations Applied to Attitude Dynamics and to the Earth Rotation. Osculating and Nonosculating Andoyer Variables [R] . Efroimsky, M. , Escapa, A. 2007

机译：经典扰动的计算和非计算andoyer变量理论在姿态动力学和地球自转中的应用。

Attitude dynamics of a spacecraft with variable structure at presence of harmonic perturbations

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