北京航空航天大学主页平台系统桂海潮--中文主页--论文成果

扫描手机二维码

欢迎您的访问
您是第位访客

开通时间：..

最后更新时间：..

登录| | 手机版

桂海潮 ( 教授 ) 赞
的个人主页 http://shi.buaa.edu.cn/guihaichao/zh_CN/index.htm
教授

论文成果当前位置：中文主页 >> 论文成果

[21] .H. Gui*, G. Vukovich, S. Xu, “Attitude Stabilization of a Spacecraft with Two Parallel Control Moment Gyros,” Journal of Guidance, Control, and Dynamics, 2016, 39(3): 724-731
[22] .H. Gui, G. Vukovich*, “Dual-Quaternion-Based Adaptive Motion Tracking of Spacecraft with Reduced Control Effort,” Nonlinear Dynamics, 2016, 83(1-2):597-614
[23] .H. Gui*, L. Jin, S. Xu, “Small-Time Local Controllability of Spacecraft Attitude Using Control Moment Gyros,” Automatica, 2015, 51(3): 141-148
[24] .H. Gui*, G. Vukovich, S. Xu, “Attitude Tracking of a Rigid Spacecraft Using Two Internal Torques,” IEEE Transactions on Aerospace and Electronic Systems, 2015, 51(4): 2900-2913
[25] .H. Gui*, L. Jin, S. Xu, J. Zhang, “On the Attitude Stabilization of a Rigid Spacecraft by Two Skew Control Moment Gyros,” Nonlinear Dynamics, 2015, 79(3): 2079-2097
[26] .H. Gui, L. Jin*, S. Xu, “Simple Finite-Time Attitude Stabilization Laws for Rigid Spacecraft with Bounded Inputs,” Aerospace Science and Technology, 2015, 42: 176-186
[27] .H. Gui, G. Vukovich*, “Adaptive Integral Sliding Mode Control for Spacecraft Attitude Tracking with Actuator Uncertainty,” Journal of the Franklin Institute, 2015, 352(12): 5832–5852
[28] .H. Gui, G. Vukovich*, “Robust Adaptive Spin-axis Stabilization of a Symmetric Spacecraft Using Two Bounded Torques,” Advances in Space Research, 2015, 56(11): 2495–2507
[29] .H. Gui, L. Jin*, S. Xu, “Maneuver Planning of a Rigid Spacecraft with Two Skew Control Moment Gyros,” Acta Astronautica, 2014, 104(1): 293-303
[30] .桂海潮*，徐世杰，金磊. 基于动态逆法的欠驱动航天器姿态机动控制[J]. 中国空间科学技术, 2014, 34(1): 1-9

共34条 3/4

首页上页下页尾页页

版权所有 2014-2022 北京航空航天大学京ICP备05004617-3 文保网安备案号1101080018
地址：北京市海淀区学院路37号邮编：100191 电话：82317114