期刊文献+
共找到2篇文章
< 1 >
每页显示 20 50 100
Theoretical analyses on bed topography responses in large depth-to-width ratio river bends with constant curvatures 被引量:1
1
作者 Shuxian GAO Haijue XU Yuchuan BAI 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI CSCD 2018年第5期747-766,共20页
Bed morphology is the result of a dynamic response to a complex meandering river system. It is an important factor for the further development of river. Based on the meandering river characterized by a large depth-to-... Bed morphology is the result of a dynamic response to a complex meandering river system. It is an important factor for the further development of river. Based on the meandering river characterized by a large depth-to-width ratio, a theoretical model is established with the coupling of Navier-Stokes (N-S)~ sediment transport, and bed deformation equations. The flow characteristics and bed response of river are obtained with the perturbation method. The research results show that, under the effect of two- dimensional flow disturbance, the bars and pools present the regular response. For a given sinuousness, the amplitude of the bed response can be used as a criterion to judge the bedform stability. The effects of the Reynolds number, disturbance wavenumber, sinuousness, and bed morphology gradient on the bed response development are described. 展开更多
关键词 meandering river large depth-to-width ratio channel disturbance wave bed response
下载PDF
Design of a robust guidance law via active disturbance rejection control 被引量:2
2
作者 Yanbo Yuan Ke Zhang 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2015年第2期353-358,共6页
Focusing on the three-dimensional guidance problem in case of target maneuvers and response delay of the autopilot, the missile guidance law utilizing active disturbance rejection control (ADRC) is proposed. Based o... Focusing on the three-dimensional guidance problem in case of target maneuvers and response delay of the autopilot, the missile guidance law utilizing active disturbance rejection control (ADRC) is proposed. Based on the nonlinear three-dimensional missile target engagement kinematics, the guidance model is es- tablished, The target acceleration is treated as a disturbance and the dynamics of the autopilot is considered by using a first-order model. A nonlinear continuous robust guidance law is designed by using a cascaded structure ADRC controller. In this method the disturbance is estimated by using the extended state observer (ESO) and compensated during each sampling period. Simulation results show that the proposed cascaded loop structure is a viable solution to the guidance law design and has strong robustness with respect to target maneuvers and response delay of the autopilot. 展开更多
关键词 three-dimensional guidance active disturbance rejection control target maneuver autopilot response delay
下载PDF
上一页 1 下一页 到第
使用帮助 返回顶部