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Free return circumlunar trajectories from launch windows with fixed launch azimuths

机译：从带有固定发射方位角的发射窗口免费返回绕月轨迹

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摘要

Earth parking orbits and free return circumlunar trajectories from launch windows with fixed azimuths - apollo project

机译：带有固定方位角的发射窗口的地面停车轨道和自由返回绕月轨迹-阿波罗计划

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Johnson F. Jr.;
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年度 1963
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1. High-latitude-landing circumlunar free return trajectory design [J] . Yim Shing Yik, Baoyin Hexi Aircraft engineering . 2015,第4期

机译：高纬度着陆绕月球的自由返回轨迹设计
2. Evaluation and selection of missile's optimal initial launch azimuth under side window detection using a hybrid decision making method [J] . Yu Ying, Hou Mingshan, Liu Bojun Aerospace science and technology . 2018,第MAY期

机译：基于混合决策方法的侧窗检测下导弹最优初始发射方位角的评估与选择
3. Ascent trajectory optimization for air-breathing vehicles in consideration of launch window [J] . Optimal Control Applications and Methods . 2020,第2期

机译：考虑到发射窗口时上升轨迹优化空气呼吸轨道
4. United Trajectory Design Method for Return to Launch Site of Suborbital Reusable Launch Vehicle [C] . Qiao Hao, Sun Peng, Li Xinguo AIAA international space planes and hypersonic systems and technologies conference . 2017

机译：亚轨道可重复使用运载火箭返回发射场的联合弹道设计方法
5. A fixed-point framework for launch vehicle ascent guidance. [D] . Zhang, Lijun. 2006

机译：运载火箭上升指导的定点框架。
6. FAILURES-TO-LAUNCH AND BOOMERANG KIDS: CONTEMPORARY DETERMINANTS OF LEAVING AND RETURNING TO THE PARENTAL HOME [O] . Scott J. South, Lei Lei -1

机译：发射失败和勃艮第的孩子：离开并返回父母家庭的当代决定因素
7. Return and abort trajectory optimisation for reusable launch vehicles [O] . Toso Federico, Maddock Christie 2017

机译：可重复使用运载火箭的返回和中止轨迹优化

Free return circumlunar trajectories from launch windows with fixed launch azimuths

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