北京航空航天大学主页平台系统胡庆雷--中文主页-- Q. Hu and X. Tan, "Dynamic Near-Optimal Control Allocation for Spacecraft Attitude Control Using a Hybrid Configuration of Actuators," IEEE Transactions on Aerospace and Electronic Systems, vol. 56, no. 2, pp. 1430-1443, April 2020.

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：..

同专业博导

同专业硕导

胡庆雷 ( 教授 ) 赞
的个人主页 http://shi.buaa.edu.cn/huqinglei/zh_CN/index.htm
教授博士生导师硕士生导师

论文当前位置：中文主页 >> 论文

Q. Hu and X. Tan, "Dynamic Near-Optimal Control Allocation for Spacecraft Attitude Control Using a Hybrid Configuration of Actuators," IEEE Transactions on Aerospace and Electronic Systems, vol. 56, no. 2, pp. 1430-1443, April 2020.

点击次数：
是否译文：否

上一条： Q. Hu, T. Han and M. Xin, "Three-Dimensional Guidance for Various Target Motions With Terminal Angle Constraints Using Twisting Control," IEEE Transactions on Industrial Electronics, vol. 67, no. 2, pp. 1242-1253, Feb. 2020.

下一条： Q. Hu, X. Shao and W. Chen, "Robust Fault-Tolerant Tracking Control for Spacecraft Proximity Operations Using Time-Varying Sliding Mode," IEEE Transactions on Aerospace and Electronic Systems, vol. 54, no. 1, pp. 2-17, Feb. 2018.