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Optimization of launch azimuth range to adjust launch window duration and improve launch vehicle performance margin

机译：优化发射方位角范围，以调整发射窗口持续时间并提高运载火箭的性能余量

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作者
Caldwell, S. F.; Martersteck, K. E.;
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年度 1970
页码 1-9
总页数 9
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
APOLLO FLIGHTS; LAUNCH WINDOWS; LUNAR LAUNCH; SPACECRAFT LAUNCHING; AZIMUTH; LUNAR TOPOGRAPHY; TIME;

机译：阿波罗航班;推出WINDOWs; LUNaR LaUNCH;航天发射;方位角;月球地形;时间;

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1. Exploring the Possibilities for Improving the Performance of the Adapters used for Launching Multiple Small Space Vehicles on a Single Launch Vehicle [J] . Viktor Nikolaevich Blinov, Viktor Vladimirovich Shalay, Igor Sergeevich Vavilov Indian Journal of Science and Technology . 2016,第27期

机译：探索提高单个运载火箭上用于发射多个小型航天器的适配器性能的可能性
2. Multidisciplinary design of air launched satellite launch vehicle: Performance comparison of heuristic optimization methods [J] . Amer Farhan Rafique, rnHe LinShu, rnAli Kamran, Acta astronautica . 2010,第7a8期

机译：空中卫星运载火箭的多学科设计：启发式优化方法的性能比较
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. Optimization of initial launching azimuth of missile under side window detection [C] . Ying Yu, Mingshan Hou, Sizhe Zhang, IEEE Chinese Guidance, Navigation and Control Conference . 2016

机译：侧窗检测下导弹初始发射方位角的优化
5. Maximum-range trajectories for an unpowered reusable launch vehicle. [D] . Bryan, Josiah A. 2011

机译：无动力可重复使用运载火箭的最大射程轨迹。
6. Lessons learned launching an engaging patient portal: an exploratory case study examining the launch and integration of the patient portal into the continuum of care for substance use treatment [O] . Michael J. Tkach, Janelle Wesloh 2020

机译：汲取的经验教训启动了一个引人入胜的患者门户网站：一项探索性案例研究检查了患者门户网站的启动以及将其整合到物质使用治疗的持续护理中
7. Three-dimensional trajectory optimization for multi-stage launch vehicle mission using a full-space quasi-Lagrange–Newton method [O] . Feng-Nan Hwang 2019

机译：使用全空间拟拉格朗日 - 牛顿方法的多级发射车任务三维轨迹优化
8. The effects of changing the launch azimuth limits on the launch window, launch vehicle payload, and communications and tracking coverage [R] . Hoekstra, T. B. 1967

机译：改变发射方位角限制对发射窗口，运载火箭有效载荷以及通信和跟踪覆盖范围的影响

Optimization of launch azimuth range to adjust launch window duration and improve launch vehicle performance margin

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