发表机构
Advanced Space, LLC（Advanced Space有限责任公司）
机构由 AI 辅助整理，请以论文原文为准。AI 中文总结
该研究提出纯凸规划方法，设计适用于地月轨道被动安全脉冲交会与接近操作的机动，验证其在NASA CAPSTONE 02任务中的性能，为星上自主制导提供基线方案。
AI 中文摘要
本文提出了用于地月轨道中被动安全脉冲交会与接近操作的纯凸规划方法。 approach、arrival和abort机动均在机动执行误差与导航不确定性的背景下设计并验证，且针对自主场景下的高效星上执行进行了公式化。所概述的方法构成了NASA CAPSTONE 02任务的基线星上制导程序，该任务计划在南部9:2会合近直线晕轨道中演示自主交会与接近操作能力。使用计划的相对导航传感器套件和测量节奏进行的高保真闭环蒙特卡洛模拟验证了预期的机动设计性能。
英文摘要
This paper presents purely convex programs for passively safe impulsive rendezvous and proximity operations in cislunar orbits. Approach, arrival, and abort maneuvers are all designed and validated in the context of maneuver execution error and navigation uncertainty, and formulated for efficient onboard execution in the autonomous scenario. The outlined methods form the baseline onboard guidance routines for NASA's CAPSTONE 02 mission planned to demonstrate autonomous rendezvous and proximity operations capabilities in the southern 9:2 synodic near rectilinear halo orbit. High fidelity closed loop Monte Carlo simulations using the planned relative navigation sensor suite and measurement cadence verify the intended maneuver design performance.
CommentsPresented at the 2026 AAS/AIAA Astrodynamics Specialist Conference, Whistler, BC
