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一种多旋翼无人机回收装置 专利
专利类型: 发明, 专利号: CN111348186A, 公开日期: 2020-06-30,
Inventors:  何玉庆;  杨丽英;  朱建龙;  余鑫鑫;  孙晓舒
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一种发动机硬件在回路仿真系统 专利
专利类型: 发明, 专利号: CN111290289A, 公开日期: 2020-06-16,
Inventors:  何玉庆;  杨丽英;  李思梁;  黄朝雄;  孙晓舒
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一种无人机空中回收系统 专利
专利类型: 发明, 专利号: CN111284722A, 公开日期: 2020-06-16,
Inventors:  何玉庆;  谷丰;  周浩;  杨丽英;  于利;  常彦春;  孙晓舒;  余鑫鑫
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A study of flexible flow shop scheduling problem with variable processing times based on improved bat algorithm 期刊论文
International Journal of Simulation and Process Modelling, 2020, 卷号: 15, 期号: 3, 页码: 245-254
Authors:  Bian, Jianyong;  Yang LY(杨丽英)
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flexible flow shop  bat algorithm  BA  variable processing time  Hamming distance  adaptive position update  
飞行机械臂系统的接触力控制 期刊论文
控制理论与应用, 2020, 卷号: 37, 期号: 1, 页码: 59-68
Authors:  孟祥冬;  何玉庆;  张宏达;  杨丽英;  谷丰;  韩建达
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飞行机械臂  接触操作  接触力控制  阻抗控制  弹簧-质量-阻尼系统  
基于多站测距定位的无人直升机自主降落引导方法研究 期刊论文
航空兵器, 2020, 页码: 1-7
Authors:  潘思;  谷丰;  狄春雷;  常彦春;  杨丽英;  何玉庆
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多站测距定位  自主降落  加权最小二乘定位法  扩展卡尔曼滤波  随机海浪模型  
Mode Transition Control of Dual Tilt Rotor Unmanned Aerial Vehicle Based on Dynamic Analysis 会议论文
Proceedings of the 32nd Chinese Control and Decision Conference, CCDC 2020, Hefei, China, August 22-24, 2020
Authors:  Zheng RJ(郑锐剑);  He YQ(何玉庆);  Liu Z(刘重);  Yang LY(杨丽英);  Gu F(谷丰)
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Tilt Rotor  Unmanned Aerial Vehicle  Dynamic Analysis  Model Transition Control  Passivity  
结合滤波与优化的无人机多传感器融合方法 期刊论文
中国科学:信息科学, 2020, 页码: 1-13
Authors:  代波;  何玉庆;  谷丰;  杨丽英;  徐卫良
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无人机  传感器融合  状态估计  卡尔曼滤波  全局优化  
Interconnection and Damping Assignment Passivity-Based Control Design Under Loss of Actuator Effectiveness 期刊论文
Journal of Intelligent and Robotic Systems: Theory and Applications, 2020, 卷号: 100, 期号: 1, 页码: 29-45
Authors:  Liu Z(刘重);  Theilliol, Didier;  Yang LY(杨丽英);  He YQ(何玉庆);  Han JD(韩建达)
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IDA-PBC  Loss of actuator effectiveness  Passive FTC  RUAV  
Wind disturbance rejection for unmanned aerial vehicles using acceleration feedback enhanced H∞ method 期刊论文
Autonomous Robots, 2020, 页码: 15
Authors:  Dai B(代波);  He YQ(何玉庆);  Zhang GY(张广玉);  Gu F(谷丰);  Yang LY(杨丽英);  Xu WL(徐卫良)
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Wind disturbance rejection  Acceleration feedback  Unmanned aerial vehicle  H∞ control