用功能连接理论进行轨道机动的触角速度约束
A K de Almeida1, T Vaillant2,3, V M de Oliveira3,4
1CICGE, DGAOT, FCUP, Vila Nova de Gaia, Portugal. allan.junior@inpe.br.
Scientific reports
|March 30, 2024
概括
这项研究引入了一种新的方法,用于在 cislunar 空间中使用接触速度约束来操作航天器. 这种方法显著减少了设计节能轨道转移和重力辅助的计算时间.
科学领域:
- 天体动力学和太空飞行工程
- 轨道力学 轨道力学
- 计算数学 计算数学 计算数学
背景情况:
- 由于地球,月球和太阳的引力扰动,在西斯隆太空中机动的航天器是复杂的.
- 燃油效率高的轨迹对于减少有效载荷质量至关重要.
- 传统的两点边界值问题 (TPBVP) 用于轨迹设计,但可能是计算密集的.
研究的目的:
- 提出和评估一种新的方法来设计使用触速 (TV) 约束的轨道机动.
- 为了证明功能连接理论 (TFC) 在解决空间任务设计的电视约束方面的效率.
- 将电视约束的计算性能与传统的TPBVP方法进行比较.
主要方法:
- 使用触速 (TV) 约束的轨道机动的数学建模.
- 运用功能连接理论 (TFC) 来嵌入和解决这些电视约束.
- 优化技术,包括与TFC集成的非线性最小平方.
主要成果:
- 通过TFC解决的拟议的电视约束方法,有效地设计了轨道转移 (例如,地球到月球) 和重力辅助机动 (例如,月球旋转).
- 与传统的TPBVP方法相比,计算时间显著减少.
- 证明TFC的效率和有效性,用于推断复杂的轨道转移.
结论:
- 触角速度约束为设计在 cislunar 空间中的航天器机动提供了一个有效的替代方案.
- TFC 方法为解决这些机动提供了一个计算上有利的方法.
- 这种技术增强了燃料效率高的太空任务的设计过程.
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