空间控制技术与应用（中英文）2026，Vol.52Issue(4)：43-52,10.DOI:10.3969/j.issn.1674-1579.2026.04.005
基于太阳帆与洛伦兹力在木星附近编队构型保持控制
Formation Keeping Control Near Jupiter Based on Solar Sails and Lorentz Force
摘要
Abstract
A propellant-free hybrid propulsion control scheme combining solar sail photon pressure and Lorentz force induced by Jupiter's magnetic field is proposed in this paper to address the two-spacecraft formation flying problem in near-Jupiter orbits.It is assumed that two equal-mass solar sail spacecraft operate on near-Jupiter circular orbits,where the chief spacecraft is electrically neutral and the deputy spacecraft carries controllable net electric charge.First,under the assumption of Jupiter's central gravitational field,a linearized relative motion dynamic model in the LVLH coordinate frame is established based on the Hill-Clohessy-Wiltshire equations.Considering the distinctive dynamic environment of near-Jupiter orbits,linearized correction terms accounting for Jupiter's strong non-spherical gravitational perturbation and Lorentz force terms derived from the tilted dipole magnetic field model of Jupiter are further incorporated.The solar sail light pressure difference is treated as a 3-dimensional continuous control input,while the charge-to-mass ratio of the deputy spacecraft serves as an auxiliary scalar control input,forming a complete state-space model for hybrid propulsion.Analysis reveals that the proposed hybrid control strategy can overcome the underactuated limitation of Lorentz force control alone and achieve full-state controllability for formation configuration maintenance.This work delivers a novel propellantless control paradigm for deep-space solar sail formation missions.关键词
太阳帆/洛伦兹力/构型保持/自适应控制/木星Key words
solar sail/Lorentz force/formation keeping/adaptive control/Jupiter分类
航空航天引用本文复制引用
周奕彤,袁长清,赵磊..基于太阳帆与洛伦兹力在木星附近编队构型保持控制[J].空间控制技术与应用（中英文）,2026,52(4):43-52,10.基金项目
国家自然科学基金资助项目(11372353,10902125) State Key Program of National Natural Science of China(11372353,10902125) （11372353,10902125）
