On the Lyapunov stability of stationary points around a central body

被引:7
作者
Elipe, A. [1 ]
Lopez-Moratalla, Teodoro
机构
[1] Univ Zaragoza, Grp Mecan Espacial, E-50009 Zaragoza, Spain
[2] Real Observ Armada, San Fernando De Henares 11110, Spain
关键词
D O I
10.2514/1.17081
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
It is well known that for a satellite about the rotating Earth, in a frame fixed in the planet, there are four stationary solutions, two of which are stable in the linear sense and the other two-unstable. This result is proved by computing the eigenvalues of the linearized equations of motion. Determining the orbital stability (or Lyapunov stability) is more complicated because it requires firstly the computing of the normal form around the equilibrium and secondly the expression of this normal form in action-and-angle variables in order to apply the so-called Arnold's theorem of stability. Higher-order normal forms are necessary for some specific values. However, Arnold's theorem is useless in the presence of resonances, in which case a new technique (again related to normal forms) must be applied in order to determine the orbital stability. In this paper, we proceed symbolically, taking the harmonic coefficients as parameters. We find the Lyapunov stability diagram on the parametric plane for the stationary points. We also study resonances 2:1 and 3:1, as well as the case in which a higher-order normalization is needed. Therefore, whatever the values of the harmonic coefficients of the potential expansion are the Lyapunov stability of the stationary solutions is determined. The advantage of a symbolic analysis is that the replacement of the actual values of a planet or celestial body is sufficient to obtain the orbital stability of the stationary points. For Earth-like planets, these points are indeed stable.
引用
收藏
页码:1376 / 1383
页数:8
相关论文
共 19 条
[1]  
ARNOLD VI, 1961, SOV MATH DOKL, V2, P247
[2]   EFFECT OF ELLIPTICITY OF EQUATOR ON 24-HOUR NEARLY CIRCULAR SATELLITE ORBITS [J].
BLITZER, L .
JOURNAL OF GEOPHYSICAL RESEARCH, 1962, 67 (01) :329-+
[3]  
Deprit A., 1969, Celestial Mechanics, V1, P12, DOI 10.1007/BF01230629
[4]   STABILITY OF TRIANGULAR LAGRANGIAN POINTS [J].
DEPRIT, A .
ASTRONOMICAL JOURNAL, 1967, 72 (02) :173-&
[5]  
DEPRIT A, 1966, SPACE MATH 2, V6, P1
[6]  
DEPRIT A., 1996, REV MATEMATICA U COM, V9, P311
[7]   On the stability of equilibria in two-degrees-of-freedom Hamiltonian systems under resonances [J].
Elipe, A ;
Lanchares, V ;
Pascual, AI .
JOURNAL OF NONLINEAR SCIENCE, 2005, 15 (05) :305-319
[8]   Oscillators in resonance [J].
Elipe, A ;
Deprit, A .
MECHANICS RESEARCH COMMUNICATIONS, 1999, 26 (06) :635-640
[9]   Nonlinear stability in resonant cases:: A geometrical approach [J].
Elipe, A ;
Lanchares, V ;
López-Moratalla, T ;
Riaguas, A .
JOURNAL OF NONLINEAR SCIENCE, 2001, 11 (03) :211-222
[10]   Complete reduction of oscillators in resonance p:q [J].
Elipe, A .
PHYSICAL REVIEW E, 2000, 61 (06) :6477-6484