电光与控制, 2016, 23 (6): 50, 网络出版: 2021-01-28   

基于欧拉旋转的动能拦截器姿态控制方法

An Attitude Control Method of Kinetic Kill Vehicle Based on Eigenaxis Rotation
作者单位
武汉第二船舶设计研究所,武汉430205
引用该论文

刘巍, 陈源宝, 王旋. 基于欧拉旋转的动能拦截器姿态控制方法[J]. 电光与控制, 2016, 23(6): 50.

LIU Wei, CHEN Yuan-bao, WANG Xuan. An Attitude Control Method of Kinetic Kill Vehicle Based on Eigenaxis Rotation[J]. Electronics Optics & Control, 2016, 23(6): 50.

参考文献

[1] 张兵. 大气层外动能拦截器末制导段性能研究[D]. 长沙:国防科学技术大学, 2005. (ZHANG B. End-game performance analysis of exo-atmospheric kinetic vehicle[D]. Changsha: National University of Defense Technology, 2005. )

[2] 谷良贤, 龚春林, 郝波. 动能拦截器姿控与轨控方案设计及仿真[J]. 西北工业大学学报, 2007, 25(3): 402-405. (GU L X, GONG C L, HAO B. Design and simulation of KKV control scheme[J]. Journal of Northwestern Polytechnical University, 2007, 25(3): 402-405. )

[3] WEN J T, KREUTZ-DELGADO K. The attitude control problem[J]. IEEE Transactions on Automatic Control, 1991, 36(10): 1148-1162.

[4] 高大远, 陈克俊, 胡德文. 动能拦截器末制导控制系统建模与仿真[J]. 宇航学报, 2005, 26(4): 420-424, 435. (GAO D Y, CHEN K J, HU D W. Modeling and si-mulation of guidance and control of kinetic kill vehicle in terminal process of interception[J]. Journal of Astronautics, 2005, 26(4): 420-424, 435. )

[5] LAM Q, PAL P, HU A, et al. Robust attitude control using a joint quaternion feedback regulator and nonlinear model-follower[C]//AIAA/AAS Astrodynamics Conference, San Diego, 1996: 817-827.

[6] LIZARRALDE F, WEN J T. Attitude control without angular velocity measurement a passivity approach[J]. IEEE Transactions on Automatic Control, 1996, 41(3): 468-472.

[7] WIE B, BARBA P M. Quaternion feedback for spacecraft large angle maneuvers[J]. Journal of Guidance, Control, and Dynamics, 1985, 8(3): 360-365.

[8] TAYEBI A. Unit quaternion-based output feedback for the attitude tracking problem[J]. IEEE Transactions on Automatic Control, 2008, 53(6): 1516-1520.

[9] WIE B, WEISS H, ARAPOSTATHIS A. Quarternion feedback regulator for spacecraft eigenaxis rotations[J]. Journal of Guidance, Control, and Dynamics, 1989, 12(3): 375-380.

[10] 王峰, 曹喜滨, 张世杰. 基于欧拉旋转的在轨服务航天器姿态跟踪算法[J]. 宇航学报, 2008, 29(2): 570-575. (WANG F, CAO X B, ZHANG S J. Attitude tracking control of on-orbit-servcing[J]. Journal of Astronautics, 2008, 29(2): 570-575. )

[11] 张世杰, 王峰, 曹喜滨. 一种模型独立的拟欧拉轴航天器大角度姿态机动[J]. 航天控制, 2004, 22(5): 26-31. (ZHANG S J, WANG F, CAO X B. Model indepen-dent near eigenaxis rotation for move-to-rest spacecraft large angle maneuver[J]. Aerospace Control, 2004, 22(5): 26-31. )

[12] 朱雷鸣, 吴晓平, 李建伟, 等. 直角坐标系的欧拉旋转变换及动力学方程[J]. 海洋测绘, 2010, 30(3): 20-22, 40. (ZHU L M, WU X P, LI J W, et al. The eulers rotation and dynamic equation of rectangular coordinate system[J]. Hydrographic Surveying and Charting, 2010, 30(3): 20-22, 40. )

刘巍, 陈源宝, 王旋. 基于欧拉旋转的动能拦截器姿态控制方法[J]. 电光与控制, 2016, 23(6): 50. LIU Wei, CHEN Yuan-bao, WANG Xuan. An Attitude Control Method of Kinetic Kill Vehicle Based on Eigenaxis Rotation[J]. Electronics Optics & Control, 2016, 23(6): 50.

本文已被 1 篇论文引用
被引统计数据来源于中国光学期刊网
引用该论文: TXT   |   EndNote

相关论文

加载中...

关于本站 Cookie 的使用提示

中国光学期刊网使用基于 cookie 的技术来更好地为您提供各项服务,点击此处了解我们的隐私策略。 如您需继续使用本网站,请您授权我们使用本地 cookie 来保存部分信息。
全站搜索
您最值得信赖的光电行业旗舰网络服务平台!