[1] |
LI Qian, WANG Yankui, JIA Yuhong.
Roll oscillations over wing-body configuration with strake wings: Experiment
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(11): 526008-526008.
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[2] |
ZHANG Jie, LI Wangbin, WANG Zhengqu, PAN Jinzhu, BU Chen.
Transonic lateral departure motion characteristics of a low-aspect-ratio flying-wing model
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(11): 526340-526340.
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[3] |
WEI Kepeng, HU Jian, YAO Jianyong, XING Haochen, LE Guigao.
Fast terminal sliding mode control of neural networks for aeromechanical actuators
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(6): 624540-624540.
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[4] |
HE Wei, FANG Yongchun, LIANG Xiao, ZHANG Peng.
Design and implementation of a 2-DOF aerial manipulation system
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(2): 324280-324280.
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[5] |
YANG Qi, LIU Wei, YANG Xiaoliang, LI Hao.
Multidisplinary interactions numerical simulation for active control of delta wing rock
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(12): 124685-124685.
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[6] |
YUE Xin, YAO Jianyong.
Integral robust based asymptotic tracking control of electro-hydraulic load simulator
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(2): 420269-420278.
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[7] |
SU Erlong, LUO Jianjun, MIN Changwan.
Analysis and control of nonlinear loss of stability for longitudinal flight dynamics of hypersonic vehicle with high angle of attack
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(S1): 80-90.
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[8] |
WANG Qian, LI Qing, CHENG Nong, SONG Jingyan.
A nonlinear fault tolerant flight control method against structural damage
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(2): 637-647.
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[9] |
OUYANG Xiaoping, LI Feng, ZHU Ying, YANG Shangbao, YANG Huayong.
Nonlinear optimal feedforward compensation controller for heavy load aviation load simulator
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(2): 669-679.
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[10] |
ZHANG Bo, ZHOU Zhou, ZHU Xiaoping.
Attitude control of fly wing UAV with multi-boundary state constraints
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(9): 3105-3115.
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[11] |
LI Wei, MA Baofeng.
A modified loosely-coupled algorithm for calculation of wing rock
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(6): 1805-1813.
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[12] |
Zhang Youan;Ma Guoxin;Wang Xingping.
Time-cooperative Guidance for Multi-missiles: A Leader-Follower Strategy
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(6): 1109-1118.
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[13] |
Guo Jianguo;Zhou Jun.
Design of H∞ Control Based Nonlinear Terminal Guidance Law
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(12): 2423-2427.
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[14] |
Ma Kemao;He Fenghua.
Control Law Design of Lateral Attitude Jets for Spinning Missile
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(10): 1816-1822.
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[15] |
WU Zhong.
Nonlinear Control of Attitude and Momentum for Space Station
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2006, 27(6): 1155-1160.
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