Heliocentric Solar Sail Orbit Transfers with Locally Optimal Control Laws
Heliocentric Solar Sail Orbit Transfers with Locally Optimal Control Laws
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DOI：
10.2514/1.17297
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发表时间：
2007
影响因子：
1.6
通讯作者：
M. Macdonald;C. McInnes;B. Dachwald
中科院分区：
文献类型：
--
作者：
M. Macdonald;C. McInnes;B. Dachwald
空间机构越来越多地考虑将太阳航行用于未来的科学任务。由于主推进系统没有反应质量，在中远期出现了新的高能任务概念，如太阳极地轨道器或星际太阳顶层探测器[1，2]。任务分析中最耗时的任务之一是轨迹生成和优化。最优弹道生成是一个复杂的领域，存在许多方案；然而，这些方案通常被描述为需要良好的工程判断程度的计算密集型系统[3-6]。
Solar sailing is increasingly being considered by space agencies for future science missions. With the absence of reaction mass from the primary propulsion system arises the potential for new high-energy mission concepts in the mid to far term, such as a Solar Polar Orbiter or an Interstellar Heliopause Probe [1,2]. One of the most time consuming tasks of mission analysis is trajectory generation and optimization. Optimal trajectory generation is a complex field and many schemes exist; however, these are typically characterized as being computationally intensive systems requiring a good degree of engineering judgment [3-6].