北京亚洲成人在线一二三四五六区学报-亚洲成人在线一二三四五六区

Special Issue on Guidance and Control of Rockets

Robust Guidance Method for Reusable Rocket Landing Phase based on UMPSP

ZHANG Yonghua, WANG Zheng, WANG Shiyu, BAI Yunfei, QIU Likuan

2024, 0(0) doi: 10.13700/j.bh.1001-5965.2024.0491

[Abstract] [FullText HTML] [PDF 1440KB] [Cited By]
An adaptive improved PD controller for rigid-elastic coupled launch vehicles

JIANG Xingyu, XUE Fengfeng, JIANG Fanghua, SHI Peng, GONG Shengping

2024, 0(0) doi: 10.13700/j.bh.1001-5965.2024.0383

[Abstract] [FullText HTML] [PDF 0KB] [Cited By]
A symplectic pseudo-spectral successive convex optimization method for trajectory planning of ascent stage of exo-atmosphere launch vehicle

CHEN Hong-kun, TAN Shu-jun, CUI Meng-zhen, LIU Yu-xi

2024, 0(0) doi: 10.13700/j.bh.1001-5965.2024.0052

[Abstract] [FullText HTML] [PDF 0KB] [Cited By]
Theoretic model of flow resistance for gas-filled accumulators in liquid rockets

SHI Tong, HE Yunqin, LIANG Guozhu, PAN Hui, ZHU Pingping

2024, 0(0) doi: 10.13700/j.bh.1001-5965.2023.0748

[Abstract] [FullText HTML] [PDF 0KB] [Cited By]
Analytical solutions for ascent trajectory under high angle-of-attack conditions

ZHANG Keyang, WANG Peng, YU Qi, YU Wenbin, CHEN Wanchun

2025, 51(10): 3524-3534. doi: 10.13700/j.bh.1001-5965.2023.0529

[Abstract] [FullText HTML] [PDF 1233KB] [Cited By]
Numerical simulation research on opposing jet interaction characteristics of rocket inverse flight

ZHANG Pei-hong, JIA Hong-yin, ZHAO Jiao, WU Xiao-jun, ZHOU Gui-yu, ZHANG Yao-bing

2023, 0(0) doi: 10.13700/j.bh.1001-5965.2023.0710

[Abstract] [FullText HTML] [PDF 1241KB] [Cited By]
Non-cooperative automatic docking strategy of propellant umbilical connector for launch vehicle under fluctuating wind load

LI Yongyi, WANG Nan, WU Xinyue, WU Penghui, YAO Bodan

2025, 51(10): 3415-3423. doi: 10.13700/j.bh.1001-5965.2023.0506

[Abstract] [FullText HTML] [PDF 2158KB] [Cited By]
Maximum aerodynamic load prediction method during launching of vehicle launch

CHENG Huhua, WU Shuai, JIANG Zhuhui, ZHANG Rucai

2025, 51(4): 1304-1312. doi: 10.13700/j.bh.1001-5965.2023.0237

[Abstract] [FullText HTML] [PDF 976KB] [Cited By]
Rocket return trajectory tracking guidance based on convex optimization and LQR

WU Jie, ZHANG Cheng, LI Miao, XIONG Fenfen

2022, 48(11): 2270-2280. doi: 10.13700/j.bh.1001-5965.2021.0084

[Abstract] [FullText HTML] [PDF 4880KB] [Cited By]

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Founded: 1956 ( monthly )

Sponsor: Ministry of Industry and Information Technology of the People's Republic of China

Sponsored by: Beijing University of Aeronautics and Astronautics

ISSN: 1001-5965 CN: 11-2625/V

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