A study of oscillations near a resonance during the descent of a spacecraft in the atmosphere

被引：2

作者：

Zabolotnov, MY ^{[1
]}

机构：

[1] Samara State Aerosp Univ, Samara, Russia

来源：

COSMIC RESEARCH | 2003年 / 41卷 / 02期

关键词：

Atmosphere; Angle Variable; Main Resonance; Resonance Motion; Small Asymmetry;

D O I：

10.1023/A:1023339215214

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

An analysis of the stability of the resonance motion of a spacecraft with a small asymmetry during its descent in the atmosphere is carried out. In the vicinity of the main resonance, the action-angle variables are introduced and an equation of the variation of action is composed. A conclusion related to the stability of the resonance motion is made from the investigation of this equation. Sufficient conditions of stability of the resonance motion of a spacecraft are obtained and represented in a form convenient for analysis.

引用

页码：171 / 177

页数：7

共 50 条

[1] A Study of Oscillations near a Resonance during the Descent of a Spacecraft in the Atmosphere
M. Yu. Zabolotnov
Cosmic Research, 2003, 41 : 171 - 177
[2] Estimation of the Probability of Capture into a Resonance Mode of Motion for a Spacecraft during Its Descent in the Atmosphere
V. M. Belokonov
M. Yu. Zabolotnov
Cosmic Research, 2002, 40 : 467 - 478
[3] External stability of a resonance during the descent of a spacecraft with a small variable asymmetry in the martian atmosphere
Lyubimov, V. V.
Lashin, V. S.
ADVANCES IN SPACE RESEARCH, 2017, 59 (06) : 1607 - 1613
[4] Estimation of the probability of capture into a resonance mode of motion for a spacecraft during its descent in the atmosphere
Belokonov, VM
Zabolotnov, MY
COSMIC RESEARCH, 2002, 40 (05) : 467 - 478
[5] Optimal Control of a Spacecraft During Descent in the Martian Atmosphere
Matjushin, M. M.
Sokolov, N. L.
Ovechko, V. M.
SOLAR SYSTEM RESEARCH, 2017, 51 (07) : 566 - 572
[6] Optimal Control of a Spacecraft During Descent in the Martian Atmosphere
M. M. Matjushin
N. L. Sokolov
V. M. Ovechko
Solar System Research, 2017, 51 : 566 - 572
[7] Estimation of the Probability of Capture into Resonance and Parametric Analysis in the Descent of an Asymmetric Spacecraft in an Atmosphere
Kurkina E.V.
Lyubimov V.V.
Journal of Applied and Industrial Mathematics, 2018, 12 (3) : 492 - 500
[8] METHOD OF TWO-PARAMETERS CONTROL OF SPACECRAFT DURING DESCENT IN THE MARS ATMOSPHERE
Matyushin, Maksim M.
Razoumny, Yury N.
Ovenchko, Vladimir M.
Orlov, Dmitry A.
Scorobogatov, Oleg P.
Tyurina, Daria D.
THIRD IAA CONFERENCE ON DYNAMICS AND CONTROL OF SPACE SYSTEMS 2017, 2017, 161 : 863 - 872
[9] ON OSCILLATIONS NEAR AND AT RESONANCE IN OPEN PIPES
VANWIJIN.L
JOURNAL OF ENGINEERING MATHEMATICS, 1968, 2 (03) : 225 - &
[10] GAME-THEORETIC APPROACH TO PROBLEMS OF SPACECRAFT DESCENT CONTROL IN ATMOSPHERE .2.
ZUEV, GM
IVANIN, VM
IVANOV, YN
AUTOMATION AND REMOTE CONTROL, 1971, 32 (05) : 714 - &

← 1 2 3 4 5 →