Evolution of angular velocity for defunct satellites as a result of YORP: An initial study

被引:21
作者
Albuja, Antonella A. [1 ]
Scheeres, Daniel J. [1 ]
McMahon, Jay W. [1 ]
机构
[1] Univ Colorado, Boulder, CO 80309 USA
关键词
YORP effect; Rotational dynamics; Defunct satellites; SOLAR; ASTEROIDS; DYNAMICS;
D O I
10.1016/j.asr.2015.04.013
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Observations of defunct satellites show that these objects are generally rotating, with some having very fast rotation rates, yet the cause of these rapid rates is unknown. The observed secular change in the spin rate and spin axis orientation of asteroids is known to be caused by the Yarkovsky-O'Keefe-Radzievskii-Paddack (YORP) effect, however, its effect on inactive satellites in Earth orbit remains unexplored. This paper applies the YORP effect to defunct satellites and analyzes its effect on the spin rate and obliquity of these objects. This work uses two different satellite geometries to explore the secular change of the spin rate and obliquity caused by the YORP effect for inactive Geostationary Earth Orbit (GEO) satellites. One of the model satellites has an asymmetric geometry, which leads to the classical YORP effect as originally formulated for asteroids. The other model satellite is geometrically symmetric, but relies on mass distribution asymmetry to generate the YORP effect. For both models the secular change is explored with averaged dynamics, and the solutions of the averaged theory are compared with numerical integrations of the non-averaged equations of motion. Additionally, previously published observations of inactive GEO satellites are used to estimate the YORP torque acting on those bodies. A comparison between this torque and the expected torque on a defunct satellite shows that the two are of the same order of magnitude. These results motivate further study on the YORP effect in the realm of inactive satellites. (C) 2015 COSPAR. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:237 / 251
页数:15
相关论文
共 33 条
[1]   Space debris mitigation in geosynchronous orbit [J].
Anselmo, L. ;
Pardini, C. .
ADVANCES IN SPACE RESEARCH, 2008, 41 (07) :1091-1099
[2]  
Ariafar S, 2005, ESA SP PUBL, V587, P681
[3]  
Flohrer T, 2014, 1 EUR SPAC OP CTR, V1
[4]   Coupled orbit-attitude motion of high area-to-mass ratio (HAMR) objects including efficient self-shadowing [J].
Frueh, Carolin ;
Jah, Moriba K. .
ACTA ASTRONAUTICA, 2014, 95 :227-241
[5]   Coupled orbit-attitude dynamics of high area-to-mass ratio (HAMR) objects: influence of solar radiation pressure, Earth's shadow and the visibility in light curves [J].
Frueh, Carolin ;
Kelecy, Thomas M. ;
Jah, Moriba K. .
CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY, 2013, 117 (04) :385-404
[6]  
Gilmore D. G., 2002, SPACECRAFT THERMAL C
[7]  
IADC/WG4, 2007, IADCWG4
[8]  
Karavaev YuS., 2004, ADV ASTRONAUTICAL SC, V119, P1457
[9]  
Krag H., 2014, SPACEOPS C PAS CA
[10]   The internal structure of asteroid (25143) Itokawa as revealed by detection of YORP spin-up [J].
Lowry, S. C. ;
Weissman, P. R. ;
Duddy, S. R. ;
Rozitis, B. ;
Fitzsimmons, A. ;
Green, S. F. ;
Hicks, M. D. ;
Snodgrass, C. ;
Wolters, S. D. ;
Chesley, S. R. ;
Pittichova, J. ;
van Oers, P. .
ASTRONOMY & ASTROPHYSICS, 2014, 562