Process / pipelineCelestial Mechanics
轨道确定（朗伯问题）
朗伯问题（Lambert's problem）是一个经典的轨道力学边界值问题，用于在给定转移时间的情况下，确定连接空间中两点的轨道。该问题由约翰·海因里希·朗伯（Johann Heinrich Lambert）在18世纪提出，对于行星际任务和航天器机动轨迹设计至关重要。其解提供了在两个位置之间转移所需的轨道要素和速度。
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来源
- Lambert, J. H. (1761). Acta Helvetica. Physico-Mathematico-Anatomico-Botanico-Medica. link ↗
- Vallado, D. A., Crawford, P., Hujsak, R., & Kelso, T. S. (2006). Revisiting Spacetrack Report #3. In AIAA/AAS Astrodynamics Specialist Conference. DOI: 10.2514/6.2006-6753 ↗
- Gooding, R. H. (1990). A procedure for the solution of Lambert's orbital boundary-value problem. Celestial Mechanics and Dynamical Astronomy, 48(2), 145-165. DOI: 10.1007/bf00049511 ↗
如何引用本页
ScholarGate. (2026, June 3). Orbit Determination via Lambert's Problem. ScholarGate. https://scholargate.app/zh/applied-physics/orbit-determination
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