重点RelativePositionandAtti精.docx

1、重点RelativePositionandAtti精 鄂尔多斯市昊华精煤有限责任公司高家梁煤矿选煤厂清理、检修溜槽及检修煤泥刮板安全技术措施编制单位:选煤厂施工单位:选煤厂2016年1月25日-2016年4月25日审批 施工单位选煤厂编制人单位意见签名施工单位负责人机电信息部调度指挥中心安全监察部机电副总工程师安全副总工程师审批意见总工程师: International Journal of Control and Automation Vol. 4, No. 4, December, 2011 15 F. Terui, “Position and Attitude Control of a

2、Spacecraft by Sliding Mode Control ”, Proceedings of the American Control Conference, (1998, pp. 217-221. 16 D. T. Stansbery and J. R. Cloutier, “Position and Attitude Control of a Spacecraft Using the StateDependent Riccati Equation Technique ”, Proceedings of the American Control Conference, (2000

3、, pp. 1867-1871. 17 P. Singla, K. Subbarao and J. L. Junkins, “ Adaptive Output Feedback Control for Spacecraft Rendezvous and Docking Under Measurement Uncertainty ”, Journal of Guidance, Control, and Dynamics, vol. 29, (2006, pp. 892-902. 18 K. Subbarao and S. Welsh, “Nonlinear Control of Motion S

4、ynchronization for Satellite Proximity Operations ”, Journal of Guidance, Control, and Dynamics, vol. 31, (2008, pp. 1284-1294. 19 M. Xin and H. Pan, “Integrated Nonlinear Optimal Control of Spacecraft in Proximity Operations ”, International Journal of Control, vol. 83, (2010, pp. 347-363. 20 M. D.

5、 J. Brown, “ Continuous and Smooth Sliding Mode Control ”, Ph.D. dissertation, University of Alabama in Huntsville, Dept. of Electrical and Computer Engineering , chap. 8, (2001, pp, 117-120. 21 B. Wie and J. Lu, “Feedback Control Logic for Spacecraft Eigenaxis Rotations Under Slew Rate and Control

6、Constraints ”, Journal of Guidance, Control, and Dynamics, vol. 18, (1995, pp. 1372-1379. 22 M. D. Lichter and S. Dubowsky, “State, Shape, and Parameter Estimation of Space Objects from Range Images ”, Proceedings of the 2004 IEEE International Conference on Robotics & Automatio n, (2004, pp. 2974-2

7、979. 23 U. Hillenbrand and R. Lampariello, “Motion and Parameter Estimation of a Free-Floating Space Object from Range Data for Motion Prediction ”, 8 th International Symposium on Artificial Intelligence, Robotics and Automation in Space, (2005 . 24 S. G. Kim, J. L. Crassidis, Y. Cheng and A.M. Fos

8、bury, “ Kalman Filtering for Relative Spacecraft Attitude and Position Estimation ”, Journal of Guidance, Control, and Dynamics, vol. 30, (2007 , pp. 133-143. 25 F. Aghili and K. Parsa, “Adaptive Motion Estimation of a Tumbling Satellite Using Laser-Version Data with Unknown Noise Characteristics ”,

9、 Proceedings of the 2007 IEEE/RSJ International Conference on Intelligent Robots and Systems, (2007 , pp. 839-846. 26 F. Aghili and K. Parsa, “ An Adaptive Vision System for Guidance of a Robotic Manipulator to Capture a Tumbling Satellite with Unknown Dynamics ”, Proceedings of the 2008 IEEE/RSJ In

10、ternational Conference on Intelligent Robots and Systems, (2008 , pp. 839-846. 27 Y. B. Shtessel and J. M. Buffington, “Continuous Sliding Mode Control ”, Proceedings of the American Control Conference, (1998, pp. 562-563. 28 M. D. J. Brown, Y. B. Shtessel and J. M. Buffington , “ Finite Reaching Ti

11、me Continuous Sliding Mode Control with Enhanced Robustness ”, Proceedings of AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA-2000-3964. 29 G. Bartolini and P. Pydynowski, “An Improved Chattering Free, V.S.C. Scheme for Uncertain Dynamical Systems”, IEEE Transactions on Automatic

12、 Control, vol. 41, (1996, pp. 1220-1226. 30 G. Bartolini, A. Ferrara and E. Usai, “Chattering Avoidance by Second - Order Sliding Mode Control”, IEEE Transactions on Automatic Control, vol. 41, (1998, pp. 241-246. Authors LU Wei received B. E. & M. E. degrees in Spacecraft Design from the Harbin Ins

13、titute of Technology, China, in 2006 and 2008 respectively. Currently, he is a Ph. D. Candidate in Spacecraft Design from the Harbin Institute of Technology, Harbin, China. He has published about 2 refereed journal and conference papers. His research interest covers Sliding Mode Control, Robust Cont

14、rol, and Autonomous docking with a tumbling target. E-mail: luwei.spacecraft (Corresponding Author. 21 International Journal of Control and Automation Vol. 4, No. 4, December, 2011 GENG Yunhai received B. E. degree in Engineering Mechanics from the Tongji University, M. E. degree and Ph. D degree in

15、 Spacecraft Design from the Harbin Institute of Technology, China, in 1992, 1995 and 2003 respectively. Currently, he is a Professor and doctoral advisor of Spacecraft Design, Harbin Institute of Technology, China. He has published about 60 refereed journal and conference papers. His research intere

16、st covers Spacecraft Attitude and Orbit Control , and Spacecraft Dynamics Navigation Guidance and Control (GNC technology. E-mail: gengyh. CHEN Xueqin received B. E. degree in Automation, M. E. degree in Spacecraft Design and Ph. D degree in Control Science & Engineering from the Harbin Institute of

17、 Technology, China, in 2003, 2005 and 2008 respectively. Currently, she is a lecture of Spacecraft Design, Harbin Institute of Technology, China. She has published about 20 refereed journal and conference papers. Her research interest covers fault diagnosis and fault-tolerant control. E-mail: cxqhit

18、. ZHANG Fan received B. E. degree in Automation and M. E. degree in Spacecraft Design from the Harbin Institute of Technology, China, in 2008 and 2010 respectively. Currently, he is a Ph. D. Candidate in Control Science & Engineering from the Harbin Institute of Technology, Harbin, China. He has published about 3 refereed journal and conference papers. His research interest covers Coordinated Control, Spacecraft Formation Flying. E-mail: autoctrllab. 22