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            Trajectory Optimization for Guided Rockets with Impact Angle Constraint
            作者:Tingting Zhang Haoping She
            來源:本站原創
            更新時間:2013/1/15 11:15:00
            正文:

                            Beijing Institute of  Technology, Beijing, China,100081
                                  Beijing Institute of  Technology, Beijing, China,100081

             

             

            Acknowledgment
            Tingting Zhang wishes to thank Haoping She for the guidance in research and writing. Tingting Zhang thanks Shulong Guo for the technical support. Tingting Zhang thanks Yi He and Xueying Ning. This work was supported in part by Haoping She.
            References
            Lu P, DomanB D, Schierman J D, Adaptive terminal guidance for hypervelocity impact in specifed direction, Journal of Guidance, Contro, and Dynamic, vol.29, pp.269-278, 2006.
            Had N, Balakrishnan S N, Impact time and angle guidance with sliding mode, AIAA, pp. 2009-5897, 2009.
            Ratnoo A, Ghose D, Impact angle constrained interception of  stationary targets,  Jounral of Guidance,  Control, and Dynamics, vol.31, pp.1186—1821, 2008.
            Chen Xing-lin, Hua Wen-hua, Ground target interception proportional navigation law with terminal constraints, Journla of Ballistics, vol. 22, pp. 15-18, 2010.
            A. Ratnoo and D. Ghose, Impact Angle Constrained Interception of Stationary Targets, Journal of Guidance, Control, and Dynamics, vo.31, pp. 1816-1821, Nov.–Dec.2008.
            I. R. Manchester, A. V. Savkin, Circular navigation guidance law for precision missile/target engagements, Proceedings of the 41st IEEE Conference on Decision and Control, Las Vegas, USA, 2002.
            I. R. Manchester, A. V. Savkin, Circular navigation missile guidance with incomplete information and uncertainty, AIAA- 2003-5448, 2003.
            SHE Hao-ping, GUO Shu-long, YANG Shu-xing, Circular Trajectory Guidance Law with Impact Angle Constraint Based on PNG , Journal of Beijing Institute of Technology, vol.20, pp.107-111,2011.
            GUO Shu-long, Design of Guidance Law with Terminal Impact Angle Constraints and Its Application of rockets, Beijing Institute of Technology , Beijing,2011.
             
            Tingting Zhang was born in He Nan, China, 1986. She received the Bachelor’s degree in Aeronautical and Astronautical Science and Technology in 2010 from Beijing Institute of Technology, Beijing, China.
            Mailing Address: Zhongguancun South Street, Haidian District,Beijing,No.5(Beijing Institute of Technology)

             
             
               
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