机构

• 长春光学精密机械与物... [1]
• 沈阳应用生态研究所 [1]
• 广州能源研究所 [1]
• 近代物理研究所 [1]

采集方式

• OAI收割 [4]

内容类型

• 期刊论文 [3]
• 会议论文 [1]

发表日期

• 2018 [1]
• 2017 [1]
• 2013 [1]
• 2011 [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提交时间升序提交时间降序作者升序作者降序发表日期升序发表日期降序 Envelope solitary waves and their reflection and transmission due to impurities in a granular material 期刊论文  OAI收割 CHINESE PHYSICS B, 2018, 卷号: 27, 期号: 1, 页码: 014501 作者:  Du, Wen-Qing;  Sun, Jian-An;  Yang, Yang-Yang;  Duan, Wen-Shan   |  收藏  |  浏览/下载：12/0  |  提交时间：2018/05/31 impurities  envelope solitary wave  numerical simulation   Field study on energy economic assessment of office buildings envelope retrofitting in southern China 期刊论文  OAI收割 SUSTAINABLE CITIES AND SOCIETY, 2017, 卷号: 28, 页码: 154-161 作者:  Song, Xinyan;  Ye, Cantao;  Li, Huashan;  Wang, Xianlong;  Ma, Weibin   |  收藏  |  浏览/下载：28/0  |  提交时间：2017/10/12 Building Envelope Retrofitting  Trnsys Simulation  Sensitivity Factor  Economic Analysis   Evaluating functions to describe point patterns 期刊论文  OAI收割 COMMUNITY ECOLOGY, 2013, 期号: 1, 页码: 1-7 作者:  Hanberry, B. B.;  Yang, Jian 收藏  |  浏览/下载：19/0  |  提交时间：2016/12/06 K2 functions  Pair correlation function  Point pattern  Ripley's K  Simulation envelope   Control method research on wide flight envelope aerocraft (EI CONFERENCE) 会议论文  OAI收割 2nd Annual Conference on Electrical and Control Engineering, ICECE 2011, September 16, 2011 - September 18, 2011, Yichang, China 作者:  Duan Z. 收藏  |  浏览/下载：27/0  |  提交时间：2013/03/25 The flying qualities of aerocraft was directly effected by the autopilot  for the wide flight envelope aerocraft  on the basic of analyzing the typical trajectory  the three loop autopilots of roll stability  pitch and yaw were designed  using single-mode Transient suppression method  the overload due to control surface transition deflection was avoided when control parameters changing  the verification was done by non-linear simulation. The result showed that: Under the action of the disturbance torque  the maximum roll was less than 5  the range of the aerocraft was from 13.5km to 22.4km  the max height was about 5100m  the max deviation of lateral was about 42m  the maximum elevator deflection was less than 6.5 the control law was applicable within the effective range. An autopilot design method of wide flight envelope aerocraft was provided. 2011 IEEE.