机构

• 长春光学精密机械与物... [2]
• 沈阳自动化研究所 [1]
• 广州能源研究所 [1]

采集方式

• OAI收割 [4]

内容类型

• 会议论文 [2]
• 期刊论文 [2]

发表日期

• 2022 [1]
• 2020 [1]
• 2019 [1]
• 2013 [1]

学科主题

筛选

浏览/检索结果: 共4条，第1-4条 帮助 条数/页： 5101520253035404550556065707580859095100 排序方式： 请选择题名升序题名降序发表日期升序发表日期降序提交时间升序提交时间降序作者升序作者降序 Data-driven fault diagnosis of FW-UAVs with consideration of multiple operation conditions 期刊论文  OAI收割 ISA TRANSACTIONS, 2022, 卷号: 126, 页码: 472-485 作者:  Shaojun, Liang;  Shirong, Zhang;  Yuping, Huang;  Xing, Zheng;  Jian, Cheng   |  收藏  |  浏览/下载：32/0  |  提交时间：2023/11/21 Fixed-wing UAV  Multiple operation conditions  SNN  DBSCAN  DKPCA   Rope-hook recovery system of fixed wing UAV based on FFT prediction algorithm and adaptive fuzzy PID control 会议论文  OAI收割 Beijing, China, October 13-16, 2020 作者:  Zhang MX(张洺溪);  Li Q(李琦);  Chu LL(禇玲玲);  Du XT(杜心田);  Gu F(谷丰)   |  收藏  |  浏览/下载：54/0  |  提交时间：2020/12/05 heterogeneous cross-domain collaboration  Rope-hook recovery system  fuzzy PID  the fixed wing UAV  the unmanned ship   Flocking Control of Fixed-Wing UAVs With Cooperative Obstacle Avoidance Capability 期刊论文  OAI收割 Ieee Access, 2019, 卷号: 7, 页码: 17798-17808 作者:  W.W.Zhao;  H.R.Chu;  M.Y.Zhang;  T.T.Sun;  L.H.Guo   |  收藏  |  浏览/下载：38/0  |  提交时间：2020/08/24 Fixed-wing UAV swarm,multi-agent system,flocking control,cooperative,obstacle avoidance,consensus,local information communication,multiagent systems,behaviors,algorithm,consensus,Computer Science,Engineering,Telecommunications   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：30/0  |  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.