中国科学院机构知识库网格系统: 检索

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	Longitudinal Control for Balloon-Borne Launched Solar Powered UAVs in Near-Space 期刊论文 OAI收割 JOURNAL OF SYSTEMS SCIENCE & COMPLEXITY, 2022, 卷号: 35, 期号: 3, 页码: 802-819 作者: Hu Yanpeng; Guo Jin; Meng Wenyue; Liu Guanyu; Xue Wenchao \| 收藏 \| 浏览/下载：20/0 \| 提交时间：2023/02/07 Aeroelastic model balloon-borne flight test flight dynamic model longitudinal control numerical simulation solar powered UAV
	Functional Connectivity Predicts Individual Development of Inhibitory Control during Adolescence 期刊论文 OAI收割 CEREBRAL CORTEX, 2021, 卷号: 31, 期号: 5, 页码: 2686-2700 作者: Wang, Haiyan; Fan, Lingzhong; Song, Ming; Liu, Bing; Wu, Dongya \| 收藏 \| 浏览/下载：42/0 \| 提交时间：2021/06/15 adolescence functional connectivity inhibitory control longitudinal prediction stop signal task
	Linearized longitudinal dynamic model for tractor cruise control system 会议论文 OAI收割 10th International Conference on Computer Modeling and Simulation, ICCMS 2018, Sydney, NSW, Australia, January 8-10, 2018 作者: Wang Z(王卓); Liu ZX(刘知祥); Bai XP(白晓平); Gao L(高雷); Li ZQ(李志强) \| 收藏 \| 浏览/下载：20/0 \| 提交时间：2018/07/30 Tractor Cruise control system Longitudinal dynamic model Modular Mechanism modeling Inverse model
	Linearized longitudinal dynamic model for tractor cruise control system 会议论文 OAI收割 Sydney, NSW, Australia, January 8-10, 2018 作者: Gao L(高雷); Wang Z(王卓); Bai XP(白晓平); Liu ZX(刘知祥) \| 收藏 \| 浏览/下载：31/0 \| 提交时间：2018/07/30 Tractor Cruise control system Longitudinal dynamic model Modular Mechanism modeling Inverse model
	Longitudinal control law design and simulation of fixed-wing UAV (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 作者: Duan Z. 收藏 \| 浏览/下载：27/0 \| 提交时间：2013/03/25 Taken some fixed-wing UAV as the study object the aircraft movement was broken down into the longitudinal movement and lateral movement according to the linearized small perturbation principle the longitudinal control law design method was discussed using root locus which belonged to classical control theory. The six degrees of freedom nonlinear model simulation result shows that: the control parameters designed are reasonable the simulation profile is fully consistent with the setting profile the control effect of pitch angle loop and altitude loop meets with the indices requirements the method is mature and reliable easy to realize in engineering. (2013) Trans Tech Publications Switzerland.
	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：27/0 \| 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.
	飞行器纵向运动的性能极限及其飞行控制方法研究学位论文 OAI收割工学博士, 中国科学院自动化研究所: 中国科学院研究生院, 2012 作者: 卢頔收藏 \| 浏览/下载：101/0 \| 提交时间：2015/09/02 纵向飞行控制非最小相位 H2型性能极限 L1自适应控制神经网络 Longitudinal Flight Control Non-minimum Phase H2 Performance Limitation L1 Adaptive Control Neural Network