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浏览/检索结果: 共4条，第1-4条 帮助 限定条件 专题：北京航空航天大学    第一署名单位    第一作者单位    通讯作者单位     已选(0)清除 条数/页：5101520253035404550556065707580859095100   排序方式：请选择作者升序作者降序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 Stabilisation of positive systems with generalised disturbances 期刊论文 IET CONTROL THEORY AND APPLICATIONS, 2019, 卷号: 13, 页码: 2318-2325 作者:  Xu, Yuhan;  Qiao, Jianzhong;  Wang, Chenliang;  Guo, Lei 收藏  |  浏览/下载：4/0  |  提交时间：2019/12/30 observers  control system synthesis  linear programming  robust control  stability  nonlinear control systems  positive systems  generalised disturbances  stabilisation control problem  positive modelled disturbances  general disturbances  disturbance observer  positive disturbances  generally modelled disturbances  anti-disturbance control  positivity constraints  disturbance estimation values  system performances   Numerical study of combustion effects on the development of supersonic turbulent mixing layer flows with WENO schemes 期刊论文 COMPUTERS & FLUIDS, 2019, 卷号: 189, 页码: 82-93 作者:  Liu, Hongpeng;  Gao, Zhenxun;  Jiang, Chongwen;  Lee, Chunhian 收藏  |  浏览/下载：4/0  |  提交时间：2019/12/30 Supersonic turbulent combustion mixing  layer flows  Large eddy simulation  Positivity-preserving WENO schemes  Combustion effects   Stable Runge-Kutta discontinuous Galerkin solver for hypersonic rarefied gaseous flow based on 2D Boltzmann kinetic model equations 期刊论文 APPLIED MATHEMATICS AND MECHANICS-ENGLISH EDITION, 2017, 卷号: 38, 页码: 343-362 作者:  Su, Wei;  Tang, Zhenyu;  He, Bijiao;  Cai, Guobiao 收藏  |  浏览/下载：5/0  |  提交时间：2019/12/30 model equation  hypersonic flow  discontinuous Galerkin(DG)  conservative discretization  positivity-preserving limiter  Courant-Friedrichs-Lewy (CFL) condition   A Stable Runge-Kutta Discontinuous Galerkin Solver for Hypersonic Rarefied Gaseous Flows 会议论文 29th International Symposium on Rarefi ed Gas Dynamics (RGD), Xian, PEOPLES R CHINA, 2014-01-01 作者:  Su, Wei;  He, Bijiao;  Cai, Guobiao 收藏  |  浏览/下载：4/0  |  提交时间：2020/01/06 high-order discontinous Galerkin  positivity-preserving limiter  model equations  hypersonic flows