Fractal assessment of microaccelerations at weak damping of natural oscillation in spacecraft elastic elements. II

被引：0

作者：

Sedel'nikov A.V. ^{[1
]}

机构：

[1] Samara State Aerospace University, Samara

来源：

Russian Aeronautics (Iz VUZ) | 2007年 / 50卷 / 3期

关键词：

Fractal Dimension; Random Quantity; RUSSIAN Aeronautic; Natural Oscillation; Adequate Assessment;

D O I：

10.3103/S1068799807030154

中图分类号：

学科分类号：

摘要：

Making use of the Weierstrass-Mandelbrot fractal function, some problems connected with the adequate assessment of microaccelerations aboard a spacecraft are considered. The ranges of values for the function parameters that make it possible to simulate the quasi-static component of microaccelerations are also determined. © Allerton Press, Inc. 2007.

引用

页码：322 / 325

页数：3

共 7 条

[1] Modeling of Microaccelerations Caused by Running of Attitude-Control Engines of Spacecraft with Elastic Structural Elements
Sedelnikov, A. V.
MICROGRAVITY SCIENCE AND TECHNOLOGY, 2016, 28 (05) : 491 - 498
[2] Modeling of Microaccelerations Caused by Running of Attitude-Control Engines of Spacecraft with Elastic Structural Elements
A. V. Sedelnikov
Microgravity Science and Technology, 2016, 28 : 491 - 498
[3] Consideration of the Initial Deformation From Natural Oscillations of Large Elastic Elements of the Spacecraft When Assessing Microaccelerations From Thermal Shock Using a Two-dimensional Model of Thermal Conductivity
Sedelnikov, A., V
Serdakova, V. V.
Glushkov, S., V
Nikolaeva, A. S.
Evtushenko, M. A.
MICROGRAVITY SCIENCE AND TECHNOLOGY, 2022, 34 (02)
[4] Consideration of the Initial Deformation From Natural Oscillations of Large Elastic Elements of the Spacecraft When Assessing Microaccelerations From Thermal Shock Using a Two-dimensional Model of Thermal Conductivity
Sedelnikov A.V.
Serdakova V.V.
Glushkov S.V.
Nikolaeva A.S.
Evtushenko M.A.
Microgravity Science and Technology, 2022, 34
[5] Methods of Determining Oscillation Damping Characteristics for Elastic Elements of Systems with Many Degrees of Freedom.
Matveev, V.V.
Zin'kovskii, A.P.
Problemy Prochnosti, 1981, (04):
[6] Design of the Suboptimal Profiled Relay Control of Orientation of the Spacecraft Having Elastic Structural Elements with Regard for Two Oscillation Tones
A. S. Buryi
Yu. I. Krylov
S. V. Matsykin
Automation and Remote Control, 2002, 63 : 550 - 559
[7] Design of the suboptimal profiled relay control of orientation of the spacecraft having elastic structural elements with regard for two oscillation tones
Buryi, AS
Krylov, YI
Matsykin, SV
AUTOMATION AND REMOTE CONTROL, 2002, 63 (04) : 550 - 559

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