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Equinoctial elements for Vinti theory: Generalizations to an oblate spheroidal geometry

机译:Vinti理论的等分元素:扁球面几何的推广

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摘要

Vinti theory constructs orbits on an oblate spheroidal geometry, naturally encoding the gravitational potential of an oblate spheroid in the coordinates. Classical techniques use spherical geometry. Recent work applied Vinti theory to the relative motion problem by way of a linear dynamical model, which is nonsingular in the oblate spheroidal element space. But as with classical spherical elements, the linear mapping between classical spheroidal elements and inertial rectangular coordinates becomes singular for small eccentricities and/or inclinations in the sense of linear dependence of columns in the Jacobian. To mitigate these practical issues, the standard (spherical) equinoctial elements are chosen to inform in a natural way their generalization to a new nonsingular element set: the oblate spheroidal equinoctial orbital elements. The spherical equinoctial elements can be considered a special case of the spheroidal equinoctial elements in the same way that spherical coordinates can be considered a special case of oblate spheroidal coordinates. The new element set is defined and algorithms for converting between spheroidal equinoctial elements and inertial coordinates are derived. Similarities and differences between spheroidal and spherical equinoctial elements are emphasized for clarity, both in terms of the form of equations and geometrical interpretation. The transformations are valid away from the nearly rectilinear orbit regime and are exact except near the poles. When near the poles, the transformations match the accuracy of the approximate analytical solution, which has been developed to the third order inJ2in the literature. As a result, the singularity on the poles is completely eliminated for the first time.
机译:Vinti理论在扁球形球体上构造了轨道,自然地在坐标中编码了扁球形球体的引力。经典技术使用球形几何形状。最近的工作通过线性动力学模型将Vinti理论应用于相对运动问题,该动力学模型在扁球面空间中非奇异。但是,与经典球面元素一样,就雅各布柱中列的线性相关而言,对于小偏心率和/或倾斜度,经典球面元素与惯性直角坐标之间的线性映射变得奇异。为了减轻这些实际问题,选择了标准(球形)等角要素,以自然的方式将其推广到新的非奇异要素集:扁球形球状等距轨道要素。可以将球面等容元素视为球面等量元素的一种特殊情况,与将球面坐标视为扁球形球体坐标的一种特殊情况一样。定义了新的元素集,并推导了在球体等量元素和惯性坐标之间转换的算法。为了清楚起见,强调了球面和球面等角要素之间的异同,无论是在方程的形式还是在几何解释方面。该变换在远离直线轨道的情况下是有效的,并且除了极点附近以外都是精确的。当接近极点时,这些变换与近似解析解的精度相匹配,该近似解析解在文献中已发展为三阶。结果,第一次完全消除了极点上的奇异性。

著录项

  • 来源
    《Acta astronautica》 |2018年第12期|274-288|共15页
  • 作者单位

    Department of Aerospace Engineering and Engineering Mechanics, The University of Texas at Austin;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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