[1] |
Zhikun SUN, Zhiwei SHI, Weilin ZHANG, Zheng LI, Qijie SUN.
Effect of plasma actuator on lift-drag characteristics of high-speed airfoil
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 23-39.
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[2] |
ZHENG Hui, QIU Lei, YUAN Shenfang, YANG Xiaofei, LU Xulong, XUE Zhaopeng.
Experimental method of guided wave monitoring for high temperature airflow damage of C/C thermal protection structures
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(8): 225659-225659.
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[3] |
DU Xiaoqiong, LI Bin, LUO Linyin.
Braking vibration behavior of high strut landing gear of amphibious aircraft
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 526199-526199.
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[4] |
SUN Cong.
Development status, challenges and trends of strength technology for hypersonic vehicles
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 527590-527590.
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[5] |
LUO Shibin, MIAO Zhichao, SONG Jiawen.
Influencing factors of active cooling at leading edge of hypersonic vehicles
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(12): 627023-627023.
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[6] |
GAO Chang, LI Zhengzhou, HUANG Jiangtao, HE Yuanyuan, WU Yingchuan, LE Jialing, GUI Feng.
High-accuracy aerodynamic optimization of hypersonic vehicles based on continuous adjoint
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(7): 124490-124490.
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[7] |
LEI Pengxuan, YU Li, CHEN Dehua, LYU Binbin.
Influence of flight control law on body freedom flutter characteristics: Experimental study
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(6): 124378-124378.
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[8] |
DING Yibo, YUE Xiaokui, DAI Honghua, CUI Naigang.
Prescribed performance controller for flexible air-breathing hypersonic vehicle with considering inlet airflow constraint
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(11): 524838-524838.
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[9] |
LI Jiaxing, WANG Dayi, E Wei, GE Dongming.
Autonomous navigation technology based on optical image under large dynamic disturbance
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(11): 524907-524907.
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[10] |
LI Shuaicong, HE Ruizhi, TANG Guojian, AO Peng.
Profile tracking guidance law based on sliding mode control
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(S2): 724578-724578.
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[11] |
LIU Jing, WANG Chao, XIE Peng, ZHOU Chaoying.
Development of insect-like flapping wing micro air vehicle based on PD control
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(9): 223678-223678.
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[12] |
CHEN Bing, ZHENG Yong, CHEN Zhanglei, ZHANG Houtian, LIU Xinjiang.
A review of celestial navigation system on near space hypersonic vehicle
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(8): 623686-623686.
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[13] |
WU Dafang, LIN Lujin, WU Wenjun, SUN Chencheng.
Thermal/vibration test of lightweight insulation material for hypersonic vehicle under extreme-high-temperature environment up to 1 500℃
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(7): 223612-223612.
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[14] |
CONG Rongfei, YE Youda, ZHAO Zhongliang.
Characteristics of air-breathing hypersonic vehicle in force-pitch and free-roll coupling motion
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(4): 123588-123588.
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[15] |
ZHU Hongxu, LIU Yanbin, CAO Rui, LU Yuping, TANG Jiajun, YI Chunlun.
Feasibility analysis for underlying indictors in control performance evaluation of hypersonic vehicles
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(3): 323259-323259.
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