Modeling of Microaccelerations Caused by Running of Attitude-Control Engines of Spacecraft with Elastic Structural Elements

Sedelnikov A. V.

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Modeling of Microaccelerations Caused by Running of Attitude-Control Engines of Spacecraft with Elastic Structural Elements

机译：具有弹性结构元素的航天器姿态控制发动机的运行引起的微加速度建模

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摘要

The article deals with the task to estimate microaccelerations caused by natural oscillations of big elastic elements after impulse firing of an orientation system engine. Offered estimation is useful for development of space-system engineering intended for realization of gravity-sensitive processes. It can be applied for taking a decision about appropriateness of one or another process on the board of spacecraft.

机译：这篇文章的任务是估算定向系统发动机脉冲点火后由大弹性元件的自然振动引起的微加速度。提供的估计对于旨在实现重力敏感过程的空间系统工程的开发很有用。它可以用于决定航天器板上一个或另一个过程的适当性。

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来源
《Microgravity science and technology》 |2016年第5期|491-498|共8页
作者
Sedelnikov A. V.;
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作者单位

Samara State Aerosp Univ, Samara, Russia;

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原文格式 PDF
正文语种 eng
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关键词
Estimation of microaccelerations; Orientation engine; Oscillations of big elastic elements; Gravity-sensitive processes;

机译：微加速度估计;方向引擎;大弹性元件的振动;重力敏感过程;

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专利

1. FRACTAL ASSESSMENT OF MICROACCELERATIONS AT WEAK DAMPING OF NATURAL OSCILLATION IN SPACECRAFT ELASTIC ELEMENTS. I [J] . A. V. Sedelnikov Russian Aeronautics . 2006,第3期

机译：航天弹性元件中自然振动弱阻尼时微加速度的分形评估。一世
2. Study of Over-assessment of Microaccelerations when Using a Beam-Model of Elastic Elements [J] . A. V. Sedelnikov, D. P. Molyavko, K. I. Potienko International Review of Aerospace Engineering . 2016,第1期

机译：使用弹性元件的梁模型时对微加速度的过度评估的研究
3. Design of the suboptimal profiled relay control of orientation of the spacecraft having elastic structural elements with regard for two oscillation tones [J] . A. S. Buryi, Yu. I. Krylov, S. V. Matsykin Automation and Remote Control . 2002,第4期

机译：考虑两个振荡音调的具有弹性结构元件的航天器定向的次优轮廓中继控制设计
4. THERMAL FIELDS MODELING WITH ALLOWANCE OF MICROACCELERATIONS AT THE 'FOTON' SPACECRAFT [C] . V.I. Abrashkin, A.E. Kazakova, V.V. Vasiliev, 52nd International Astronautical Congress Oct 1-5, 2001 Toulouse, France . 2001

机译：允许在“ FOTON”空间进行微加速的热场建模
5. Heat Engines running upon a Non-Ideal Fluid Model with Higher Efficiencies than upon the Ideal Gas Model [D] . Madakavil, Abhimanyu Salin. 2016

机译：加热发动机在非理想的流体模型上运行，效率高于理想的气体模型
6. Accuracy of gastrocnemius muscles forces in walking and running goats predicted by one-element and two-element Hill-type models [O] . Sabrina S.M. Lee, Allison S. Arnold, Maria de Boef Miara, -1

机译：一元素和二元素希尔型模型预测的步行和奔跑山羊腓肠肌力的准确性
7. Thermo-elastic distortion measurements by holographic interferometry and correlation with finite element models for SiC connections/junctions on spacecraft [O] . Thizy, Cédric, Stockman, Yvan, Eliot, Fabienne, 2010

机译：全息干涉测量热弹性畸变并与航天器上SiC连接/结的有限元模型相关
8. Structural Inelasticity. XIII. Finite Element Models for Elastic-Plastic Structures. [R] . hodge,philip g. jr 1975

机译：结构无弹性。十三。弹塑性结构的有限元模型。

Modeling of Microaccelerations Caused by Running of Attitude-Control Engines of Spacecraft with Elastic Structural Elements

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