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Trajectory Control and Analysis for the Vertical Takeoff and Vertical Landing Reusable Launch Vehiclea??s Upper Stage

机译：垂直起飞和垂直着陆可重复使用运载火箭上段的弹道控制与分析

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《AIAA Guidance, Navigation, and Control Conference and Exhibit》|2005年|P.1-12|共12页
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Y. Xu;
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中图分类飞行控制系统与导航;
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专利

1. Trajectory Analysis for Vertical Takeoff and Vertical Landing Reusable Launch Vehicle's Upper Stage [J] . Yunjun Xu Journal of aerospace engineering . 2009,第1期

机译：垂直起飞和垂直着陆可重复使用运载火箭上段的弹道分析
2. Uncertainty Analysis for Return Trajectory of Vertical Takeoff and Vertical Landing Reusable Launch Vehicle [J] . Jian Zhao, Haiyang Li, Xiangyue He, Mathematical Problems in Engineering: Theory, Methods and Applications . 2020,第1期

机译：垂直起飞返回轨迹的不确定性分析和垂直着陆可重复使用的发射车辆
3. Design and dynamic analysis of landing gear system in vertical takeoff and vertical landing reusable launch vehicle [J] . Zhang Ming, Xu Dafu, Yue Shuai, Proceedings of the Institution of Mechanical Engineers . 2019,第10期

机译：垂直起飞和垂直着陆可重复使用运载火箭起落架系统的设计和动力学分析
4. PATH-CONSTRAINED OPTIMAL TRAJECTORY DESIGN FOR THE UPPER STAGE OF A VERTICAL TAKEOFF VERTICAL LANDING LAUNCH VEHICLE [C] . Yunjun Xu AAS/AIAA Space Flight Mechanics Meeting; 20070128-0201; Sedona,AZ(US) . 2007

机译：垂直起飞垂直着陆车辆上段的路径约束最优弹道设计
5. Aerodynamically controlled expansion (ACE) nozzle for short takeoff and vertical landing aircraft. [D] . Terrier, Douglas Anthony. 2000

机译：气动起飞（ACE）喷嘴，用于短距起飞和垂直降落飞机。
6. Control System for Vertical Take-Off and Landing Vehicle’s Adaptive Landing Based on Multi-Sensor Data Fusion [O] . Hongyan Tang, Dan Zhang, Zhongxue Gan 2020

机译：基于多传感器数据融合的垂直起飞和着陆车辆自适应降落控制系统
7. Recent progress on development trend and key technologies of vertical take-off vertical landing reusable launch vehicle [O] . DaFu XU, Zhe ZHANG, Ke WU, 2016

机译：近期发展趋势与垂直垂直着陆可重复使用发动机的关键技术进展

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