J(2) problem;
Rigid body;
Full two body problem;
Non-canonical Hamiltonian structure;
Reduction;
Relative equilibria;
FULL 2-BODY PROBLEM;
CENTRAL GRAVITATIONAL-FIELD;
3-BODY PROBLEM;
EULERIAN EQUILIBRIA;
STATIONARY MOTIONS;
ROTATIONAL MOTION;
ATTRACTION FIELD;
OBLATE PLANET;
DYNAMICS;
GYROSTAT;
D O I:
10.1016/j.asr.2012.10.030
中图分类号:
V [航空、航天];
学科分类号:
08 ;
0825 ;
摘要:
The J(2) problem is an important problem in celestial mechanics, orbital dynamics and orbital design of spacecraft, as non-spherical mass distribution of the celestial body is taken into account. In this paper, the J(2) problem is generalized to the motion of a rigid body in a J(2) gravitational field. The relative equilibria are studied by using geometric mechanics. A Poisson reduction process is carried out by means of the symmetry. Non-canonical Hamiltonian structure and equations of motion of the reduced system are obtained. The basic geometrical properties of the relative equilibria are given through some analyses on the equilibrium conditions. Then we restrict to the zeroth and second-order approximations of the gravitational potential. Under these approximations, the existence and detailed properties of the relative equilibria are investigated. The orbit rotation coupling of the rigid body is discussed. It is found that under the second-order approximation, there exists a classical type of relative equilibria except when the rigid body is near the surface of the central body and the central body is very elongated. Another non-classical type of relative equilibria can exist when the central body is elongated enough and has a low average density. The non-classical type of relative equilibria in our paper is distinct from the non-Lagrangian relative equilibria in the spherically-simplified Full Two Body Problem, which cannot exist under the second-order approximation. Our results also extend the previous results on the classical type of relative equilibria in the spherically-simplified Full Two Body Problem by taking into account the oblateness of the primary body. The results on relative equilibria are useful for studies on the motion of many natural satellites, whose motion are close to the relative equilibria. (c) 2012 COSPAR. Published by Elsevier Ltd. All rights reserved.
机构:
China Xian Satellite Control Ctr, State Key Lab Astronaut Dynam, Xian 710043, Peoples R China
McGill Univ, Dept Mech Engn, Montreal, PQ, CanadaChina Xian Satellite Control Ctr, State Key Lab Astronaut Dynam, Xian 710043, Peoples R China
Cao, Lu
Misra, Arun K.
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机构:
McGill Univ, Dept Mech Engn, Montreal, PQ, CanadaChina Xian Satellite Control Ctr, State Key Lab Astronaut Dynam, Xian 710043, Peoples R China
机构:
Technion Israel Inst Technol, Distributed Space Syst Lab, Fac Aerosp Engn, IL-32000 Haifa, IsraelTechnion Israel Inst Technol, Distributed Space Syst Lab, Fac Aerosp Engn, IL-32000 Haifa, Israel
Wang, Yue
Xu, Shijie
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机构:
Beijing Univ Aeronaut & Astronaut, Sch Astronaut, Beijing 100191, Peoples R ChinaTechnion Israel Inst Technol, Distributed Space Syst Lab, Fac Aerosp Engn, IL-32000 Haifa, Israel