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	Robust Adaptive Tracking Control for Hypersonic Vehicle Based on Interval Type-2 Fuzzy Logic System and Small-Gain Approach 期刊论文 OAI收割 IEEE TRANSACTIONS ON CYBERNETICS, 2021, 卷号: 51, 期号: 5, 页码: 2504-2517 作者: Tao, Xinlong; Yi, Jianqiang; Pu, Zhiqiang; Xiong, Tianyi \| 收藏 \| 浏览/下载：50/0 \| 提交时间：2021/06/07 Adaptation models Aerodynamics Adaptive systems Fuzzy logic Atmospheric modeling Control design Vehicle dynamics Adaptive control hypersonic vehicle interval type-2 fuzzy logic system (IT2-FLS) robust control small-gain approach
	Atmospheric Turbulence Suppression Algorithm Based on APD Adaptive Gain Control for FSO Links of 5G Floating Base Stations 期刊论文 OAI收割 IEEE PHOTONICS JOURNAL, 2020, 卷号: 12, 期号: 4, 页码: 11 作者: Yu, Xiaonan; Xiao, Lei; Gao, Shuaihe; Song, Yansong; Zhang, Lei \| 收藏 \| 浏览/下载：49/0 \| 提交时间：2020/08/31 Free space optical communication atmospheric turbulence avalanche photodiode adaptive gain control airship 5G base station
	Adaptive Output Regulation of a Class of Nonlinear Output Feedback Systems With Unknown High Frequency Gain 期刊论文 OAI收割 IEEE/CAA Journal of Automatica Sinica, 2020, 卷号: 7, 期号: 2, 页码: 568-574 作者: Yuan Jiang; Jiyang Dai \| 收藏 \| 浏览/下载：7/0 \| 提交时间：2021/03/11 Adaptive control backstepping high frequency gain output regulation
	Distributed Adaptive Fault-Tolerant Output Regulation of Heterogeneous Multi-Agent Systems With Coupling Uncertainties and Actuator Faults 期刊论文 OAI收割 IEEE/CAA Journal of Automatica Sinica, 2020, 卷号: 7, 期号: 4, 页码: 1098-1106 作者: Chao Deng; Weinan Gao; Weiwei Che \| 收藏 \| 浏览/下载：21/0 \| 提交时间：2021/03/11 Adaptive control cyclic-small-gain fault-tolerant control multi-agent systems (MASs)
	Augmented fixed-time observer-based continuous robust control for hypersonic vehicles with measurement noises 期刊论文 OAI收割 IET CONTROL THEORY AND APPLICATIONS, 2019, 卷号: 13, 期号: 3, 页码: 422-433 作者: \| 收藏 \| 浏览/下载：72/0 \| 提交时间：2019/07/12 linearisation techniques observers control system synthesis vehicle dynamics adaptive control aircraft control uncertain systems robust control variable structure systems space vehicles augmented fixed-time observer measurement noises cruise control flexible air-breathing hypersonic vehicles controller gains finite-time convergence fixed convergence time FAHV gain adaptation law continuous robust control input-output linearisation technique
	Adaptive Interval Type-2 Fuzzy Output Feedback Control Based on Nonlinear High Gain Observer for Flexible Air-breathing Hypersonic Vehicles 会议论文 OAI收割 Hefei, China, May 19-21, 2017 作者: Tao Xinlong; Yi Jianqiang; Yuan Ruyi; Liu Zhen \| 收藏 \| 浏览/下载：149/0 \| 提交时间：2019/05/07 Flexible Air-breathing Hypersonic Vehicle Output Feedback Control Adaptive Interval Type-2 Fuzzy Logic System Nonlinear High Gain Observer
	A Novel Vacuum System Control Strategy for High Intensity D-T Fusion Neutron Generator 期刊论文 OAI收割 JOURNAL OF FUSION ENERGY, 2016, 卷号: 35, 期号: 4, 页码: 613-620 作者: Wang, Weitian; Song, Yong; Wang, Jianye; Xu, Peng; Kong, Lingli \| 收藏 \| 浏览/下载：22/0 \| 提交时间：2017/12/13 Fusion Neutron Generator Vacuum System Control Algorithm Gain Adaptive Compensation Transfer Function
	High gain observer for drag tracking in mars entry longitudinal guidance (EI CONFERENCE) 会议论文 OAI收割 2012 International Conference on Measurement, Instrumentation and Automation, ICMIA 2012, September 15, 2012 - September 16, 2012, Guangzhou, China Wu K.; Cui H.; Ma D.; Cui P. 收藏 \| 浏览/下载：29/0 \| 提交时间：2013/03/25 An extended high gain state and perturbation observer combined with feedback linearization was applied in drag tracking for Mars entry longitudinal guidance. The observer estimates the drag the drag rate and the perturbation due to model uncertainty and disturbance for drag tracking. Mars entry simulation was performed to assess the performance of the adaptive guidance law. The results demonstrate that the proposed guidance law is robust to model error and can recover the ideal performance of the feedback linearization control. Introduction In recent years the concept of pinpoint landing has been proposed (2013) Trans Tech Publications Switzerland.
	Application research of intelligent algorithm in electric-driven flight simulation turntable (EI CONFERENCE) 会议论文 OAI收割 ISECS International Colloquium on Computing, Communication, Control, and Management, CCCM 2008, August 3, 2008 - August 4, 2008, Guangzhou, China Xie M.-J.; Wang Z.-Q.; Wang L.-M. 收藏 \| 浏览/下载：40/0 \| 提交时间：2013/03/25 Application Research of Intelligent Algorithm in Electric-driven Flight Simulation Turntable is discussed in this paper. Fuzzy control is used to solve the problem of fast tracking and overshoot since its essence belongs to PD control In order to improve the performance of system in low speed a method named variance-gain adaptive algorithm is introduced in this paper. It defines the amplifier gain as a function whose independent variable is speed so the amplifier gain can automatically be adjusted with the change of speed. When the turntable runs at low speed it has a big amplifier gain a good rigidity and high tracking accuracy. When the turntable runs at high speed the method can control the amplifier gain and ensure the system dynamic performance. Design and implementation of these algorithms is introduced in detail. Experiment results show that the Flight Simulation Turntable has achieved the required performance through using fuzzy control algorithm and variance-gain adaptive algorithm. 2008 IEEE.