论文标题
一个面内$ J_2 $ - 侵入条件和高度椭圆形卫星编队的控制算法
An In-Plane $J_2$-Invariance Condition and Control Algorithm for Highly Elliptical Satellite Formations
论文作者
论文摘要
卫星的分阶段形成提供了一种重要的手段，可以使多个卫星保持紧邻，而不会彼此危险。为了最大程度地减少将一组卫星保持在分阶段地层中所需的推进剂的量，本文为高度偏心轨道中的平面内线性线性J2-variance提供了新的条件。这里概述的维护策略与平面外运动的增长作斗争，并分析了此策略的Delta-V成本。在上下文中，本文还讨论了从这种情况和维护策略中受益的相关形式。还讨论了一个称为Boomerang Perch的高度椭圆形的栖息地。
Phased formations of satellites provide an important means of keeping multiple satellites in close proximity without becoming dangerously close to one another. In order to minimize the amount of propellant necessary to keep a set of satellites in a phased formation, this paper presents a new condition for in-plane linearized secular J2-invariance in highly eccentric orbits. A maintenance strategy outlined here combats the growth of out-of-plane motion, and the delta-v cost of this strategy is analyzed. For context, this paper also discusses relevant formations that benefit from this condition and maintenance strategy. A highly elliptical perching formation called the boomerang perch is also discussed.
