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LI Yaohua, GONG Ziyu.
Safety analysis of civil aircraft system based on improved FRAM
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(12): 324083-324083.
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YANG Zhichun, TIAN Wei, GU Yingsong, HE Shun.
Advance in the study on wing aeroelasticity with concentrated nonlinearity
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(7): 2013-2044.
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WEI Dechen, SHI Zhiwei, GENG Xi, LIU Chao, ANG Haisong.
Wind tunnel test for wing-body rock of canard-configuration aircraft
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(10): 3003-3010.
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CAO Qimeng, LI Yinghui, XU Haojun.
Stability Region of Closed-loop Pilot-vehicle System for Fly-by-wire Aircraft Based on Linear Matrix Inequalities
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(1): 19-27.
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LU Yanhui, ZHANG Shuguang.
An Improvement on PWPF Modulation of Discrete RCS and Design of the Blended Control Logic
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2012, 33(9): 1561-1570.
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Meng Jie;Xu Haojun;Zhang Jiankang.
A Comparison of Feedback and Foreback Schemes to Prevent Category Ⅱ PIO
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(9): 1701-1707.
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Zhou Qiuping;Qiu Zhiping.
Interval Analysis for Limit Cycle Flutter of a Wing with an External Store
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(3): 514-518.
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Hu Guocai;Liu Quan;Liu Xiangyi.
Influence of Nonlinear Hydraulic Lag Damper on Scaled Rotor Ground Resonance
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(11): 2182-2188.
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Yuan Kaihua;Qiu Zhiping.
Thermal Flutter Analysis of Composite Panel with Uncertain Parameters
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(1): 119-124.
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Li Daochun;Xiang Jinwu.
Effect of Control Surface Freeplay on Nonlinear Aeroelastic Responses of an Airfoil
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(8): 1385-1391.
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ZHAO Yong-hui;HU Hai-yan.
Aeroelastic Analysis of a Two-Dimensional Airfoil with Control Surface Freeplay Nonlinearity
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2003, 24(6): 521-525.
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WU Wei;FANG Zhen-ping.
ANALYSIS AND PREDICTION OF PILOT-INDUCED OSCILLATION WITH ACTUATOR RATE LIMITING OF A FLY-BY-WIRE FIGHTER AND A METHOD FOR ALLEVIATING PIO
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2002, 23(3): 231-233.
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Wang Yongxi.
EFFECT OF FLIGHT CONTROL SYSTEM ON PILOT INDUCED OSCILLATION
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1997, 18(1): 17-21.
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Cheng Zhiqing;Zhou Chuanrong;Cheng Jinsong.
LIMIT CYCLE ANALYSIS OF GROUND RESONANCE OF HELICOPTER WITH NONLINEAR DAMPING
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1994, 15(5): 552-557.
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Ye Wei-liang.
LIMIT CYCLE OSCILLATION OF A FLUTTERING PLATE
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1992, 13(9): 555-559.
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CJA
