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机译:电动系留系统脱轨的实用操作策略
a: orbital semimajor axis; B~0: geomagnetic field vector in orbital coordinate; e: orbital eccentricity; F~0: Lorenz force vector acting on tether in orbital coordinate; I: intensity of current; i:orbital inclination measured from geomagnetic equator; L~0: direction vector of tether in orbital coordinate; l: length of tether; M: mass of debris; M_r: reduced mass of EDT; M_r : Mm/(M + m); m: tip mass of EDT; Q_θ,Q_φ: generalized forces; r: orbital radius; x~I,y~I,z~I: inertia coordinate system; x~0,y~0,z~0: orbital coordinate system; θ: in-plane attitude angle; μ_m: strength of magnetic dipole; μ_g: Earth gravitational constant; v: orbital true anomaly; φ: out-of-plane attitude angle; ψ: change angle of orbital plane;
机译:卫星脱轨中柔性裸露电动系链系统的振动和横向动态稳定性控制
机译:电动束缚脱轨系统动力学和性能分析
机译:电动系泊轨道系统在椭圆轨道上的动态行为及其洛伦兹力控制。
机译:电动流变仪除臭系统的鲁棒流变仪配置控制
机译:现实的空心阴极等离子体接触器模型对裸露的电动系链系统的影响。
机译:HFF-QCM在连续气流中稳定运行的实用策略
机译:终结者TETHER™电动拖曳技术在星座航天器的应用中的应用
机译:低密度磁层中电离层以外的电动线束操作