| Citation: | Guo Zhenhua, Dong Changhong. Studies on the Overall Project Design of Missile[J]. Journal of Beijing University of Aeronautics and Astronautics, 1999, 25(6): 672-675. (in Chinese)
|
|
1. Redmon R K.Tactical missile conceptual design.Galifornia:Maval Postgraduate School,1980.93~211 2. Jensen G E,Netzer D W. Tactical missile propulsion. Virginia: AIAA Inc, 1996.5~446 3. 北航、西工大．有翼导弹总体设计原理．北京:国防工业出版社,1980.52~129 4. 阮 濂,章国栋．工程系统的规划与设计．北京:北京航空航天大学出版社,1991.348~355
|
| [1] | ZHAO Yuyu, WANG Baocheng, HUANG Tingshuang, JIA Zhongzhen, DU Xiaowei, XU Guoning. Research on Model Predictive Control Strategy for Buck-Boost Converter of Near-Space Aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0860 |
| [2] | YANG Changpeng, REN Hongyan, SUN Tengfei, ZHOU Qiang, HUANG Xing, ZHANG Lihua, XIONG Liang, SUN Ji, CHENG Wenlong. Thermal control design features and flight validation of Queqiao-2 satellite[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2025.0059 |
| [3] | WANG Y J，CHEN Q Y，GAO X Z，et al. Guidance and control method for dynamic net-recovery of UAV and the flight test verification[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（2）：487-497 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0043. |
| [4] | TAO J，CAO Y F. UAV obstacle avoidance path-following method under time-varying wind disturbance at low altitudes[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（1）：175-182 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0956. |
| [5] | WANG X L，YIN H，HE M. Potential conflict prediction of mobile targets in airfield areas based on LSTM[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（6）：1850-1860 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0505. |
| [6] | GUO Wenjuan, LI Qiang, ZHOU Ling. A CFD grid uncertainty analysis method for hypersonic aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0099 |
| [7] | LYU Yuzhu. Study on Flight Characteristics and Speed Limit of Helicopter with Slung Load[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0563 |
| [8] | LI Bowen, LEI Xiaoyong. Flight task recognition and action segmentation based on SVM[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0635 |
| [9] | YANG Jun-feng, CHENG Xuan, WANG Jian-mei, ZHANG Yi-ming, HU Xiong, XIAO Cun-ying. Research for high-altitude wind shear characteristics[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0738 |
| [10] | YANG R R，ZHANG L，ZHAO J L，et al. Nonlinear variable damping integral sliding mode control for electro-hydrostatic actuator[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（1）：163-172 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0252. |
| [11] | XU H，HAN J L，XI Y，et al. Aeroelastic morphing flight simulation platform for a folding wing aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（6）：1921-1930 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0536. |
| [12] | ZUO L，ZHANG X L，LI Z Y，et al. UAV control law design method based on active-disturbance rejection control[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（5）：1512-1522 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0488. |
| [13] | LEI Juan-mian, ZHU Pei-yu. Numerical Study on Lateral Jet Control Efficiency of Hypersonic Reentry Double-cone Vehicle[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0714 |
| [14] | LIU S S，LUO L，HAN Q H，et al. Study on lateral-directional stability of a practical high lift-to-drag ratio hypersonic vehicle with momentum lift augmentation[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（11）：3010-3021 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0035. |
| [15] | WANG Y W，LEI R W，WANG H. Structural topology optimization of flying wing aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（2）：482-490 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0262. |
| [16] | JIN Z B，LI D C，SUN Y，et al. Man-machine cooperative control of helicopter and flight experimental validation[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（11）：3022-3030 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0038. |
| [17] | YANG Shang-hang, XU Guo-ning, JIA Zhong-zhen, LI Yong-xiang, ZHUANG Chun-yu, YANG Yan-chu. Research on wireless charging coil location method of aircraft based on machine learning[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023-0006 |
| [18] | YANG Yuchen, ZHANG Zenghui, YAN Jianing, ZHANG Jing, YANG Lingyu. Dual-channel control of hypersonic flight vehicles based on bounded perturbation analysis of eigenvalues[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(10): 2020-2030. doi: 10.13700/j.bh.1001-5965.2021.0053 |
| [19] | ZHANG Yuan, HUANG Wanwei, LU Kunfeng, BAI Wenyan, YU Jianglong. Modeling and finite-time control for hypersonic morphing flight vehicle[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(10): 1979-1993. doi: 10.13700/j.bh.1001-5965.2021.0701 |
| [20] | WU Wenhao, ZHANG Xuejun, GU Bo, ZHU Xiaohui. A global network flight flow assignment algorithm based on civil-military integration[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(9): 1926-1932. doi: 10.13700/j.bh.1001-5965.2018.0006 |
Copyright © Journal of Beijing University of Aeronautics and Astronautics
Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn
Supported by:
Beijing Renhe Information Technology Co., Ltd.
Lu Zixing, Liu Zixian. Elastic properties for 3 dimensional and 5 directional braided composites[J]. Journal of Beijing University of Aeronautics and Astronautics, 2006, 32(04): 455-460. (in Chinese)
DownLoad: