This paper studies the relative orbital motion of a charged object near a spacebornemagnetic dipole, which indicates that the Lorentz force acting on the charged object is taken into consideration. Assuming that a space station in a Keplerian circular reference orbit is capable of generating a rotating magnetic dipole (the axis of the dipole is in the direction of the orbital radius vector) and a constantly charged object moves nearby in the artificial magnetic field, a nonlinear dynamical model of the proposed relative orbital motion, which is similar to the scenario of satellite formation flying, is established based on the Hill-Clohessy-Wiltshire (HCW) equation. Moreover, we suppose that the Lorentz force acts on the charged object only and does not affect the circular reference orbit of the spaceborne magnetic dipole. Based on the system parameters such as the charge-to-mass ratio of the charged object, magnetic dipole's moment and rotating rate, and the angular velocity of the circular reference orbit, we firstly derived system's equilibrium points and analyzed their stabilities. Subsequently, an integral constant and the zero-velocity surfaces of the dynamical system are derived, and it is clear to show the presence of bounded orbits around the magnetic dipole and transient orbits through equilibrium points. The flight mechanics of presented relative orbital motion, including equilibrium points andzero-velocity surfaces, reveals prospects of potential applications for proximity operations to a wide range of charged space objects.
PENG Chao, GAO Yang
. Equilibrium Points and Zero-Velocity Surfaces in the Presence of Inter-Satellite Lorentz Force[J]. Journal of Deep Space Exploration, 2015
, 2(3)
: 246
-255
.
DOI: 10.15982/j.issn.2095-7777.2015.03.010
[1] Folta D C,Newman L K,Gardner T.Foundations of formation flying for mission to planet earth and the new millennium[C]//Proceedings of the AIAA/AAS Astrodynamics Conference C. [S.l.]: AIAA, 1996:656-666.
[2] Roux A. Cluster regroups for relaunch[J]. Aerospace America, 1998,36 (8):48-51.
[3] Folkner W M, Hechlerz F, Sweetsery T H, et al. LISA orbit selection and stability[J]. Classical and Quantum Gravity, 1997,14(6):1405-1410.
[4] Koss J, Pohlig S, Trichel M, et al.Precision radar surveillance and mapping with discovererⅡ[C]//Proceedings of the AIAA Space Technology Conference and Exposition C.[S.l.]: AIAA, 1999:99-4570.
[5] Peck M A. Lorentz-actuated orbits: electrodynamic propulsion without a tether[R].NASA Institute for Advanced Concepts, Phase I Final Report, 2006.
[6] Schaffer L, Burns J A. The dynamics of weakly charged dust: motion through Jupiter's gravitatinal and magnetic fields[J]. Journal of Geophysical Research, 1987(92):2264-2280.
[7] Hough M E. Lorentz force perturbations of a charged ballistic missile[C]//Proceedings of AIAA Guidance and Control Conference. USA: AIAA, 1982:227-287.
[8] Streetman B, Peck M A. New synchronous orbits using the geomagnetic Lorentz force[J]. Journal of Guidance,Control, and Dynamics, 2007,30(6):1677-1690.
[9] Schaub H, Junkins J L. Analytical mechanics of space systems[M]. USA: American Institute of Aeronautics and Astronautics, 2003.
