Element sets for high-order Poincar, mapping of perturbed Keplerian motion

被引:7
作者
Gondelach, David J. [1 ]
Armellin, Roberto [1 ]
机构
[1] Univ Surrey, Surrey Space Ctr, Guildford GU2 7XH, Surrey, England
关键词
Poincare map; Stroboscopic map; Orbit propagation; Orbit element sets; ARTIFICIAL SATELLITE THEORY; ORBITS; DYNAMICS;
D O I
10.1007/s10569-018-9859-z
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
The propagation and Poincar, mapping of perturbed Keplerian motion is a key topic in Celestial Mechanics and Astrodynamics, e.g., to study the stability of orbits or design bounded relative trajectories. The high-order transfer map (HOTM) method enables efficient mapping of perturbed Keplerian orbits using the high-order Taylor expansion of a Poincar, or stroboscopic map. The HOTM is only accurate close to the expansion point and therefore the number of revolutions for which the map is accurate tends to be limited. The proper selection of coordinates is of key importance for improving the performance of the HOTM method. In this paper, we investigate the use of different element sets for expressing the high-order map in order to find the coordinates that perform best in terms of accuracy. A new set of elements is introduced that enables extremely accurate mapping of the state, even for high eccentricities and higher-order zonal perturbations. Finally, the high-order map is shown to be very useful for the determination and study of fixed points and center manifolds of Poincar, maps.
引用
收藏
页数:35
相关论文
共 44 条
[11]   SOLUTION OF THE PROBLEM OF ARTIFICIAL SATELLITE THEORY WITHOUT DRAG [J].
BROUWER, D .
ASTRONOMICAL JOURNAL, 1959, 64 (09) :378-397
[12]   FROZEN ORBITS FOR SATELLITES CLOSE TO AN EARTH-LIKE [J].
COFFEY, SL ;
DEPRIT, A ;
DEPRIT, E .
CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY, 1994, 59 (01) :37-72
[13]  
Deprit A., 1969, Celestial Mechanics, V1, P12, DOI 10.1007/BF01230629
[14]   IDEAL ELEMENTS FOR PERTURBED KEPLERIAN MOTIONS [J].
DEPRIT, A .
JOURNAL OF RESEARCH OF THE NATIONAL BUREAU OF STANDARDS SECTION B-MATHEMATICAL SCIENCES, 1975, 79 (1-2) :1-15
[15]  
Deprit A., 1970, Celestial Mechanics, V2, P166, DOI 10.1007/BF01229494
[16]   LINEARIZATION - LAPLACE VS STIEFEL [J].
DEPRIT, A ;
ELIPE, A ;
FERRER, S .
CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY, 1994, 58 (02) :151-201
[17]   Application of high order expansions of two-point boundary value problems to astrodynamics [J].
Di Lizia, P. ;
Armellin, R. ;
Lavagna, M. .
CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY, 2008, 102 (04) :355-375
[18]  
Dunham DW, 2003, PROCEEDINGS OF THE CONFERENCE ON LIBRATION POINT ORBITS AND APPLICATIONS, P45
[19]   Dynamics of artificial satellite orbits with tesseral resonances including the effects of luni-solar perturbations [J].
Ely, TA ;
Howell, KC .
DYNAMICS AND STABILITY OF SYSTEMS, 1997, 12 (04) :243-269
[20]  
Finkleman D., 2014, 65 INT ASTR C TOR CA