HE Ying?xi.The present situation and prospect of foreign terminal sensing ammunition[J].Projectile & Rocket Technology,1995(2):1-11.(in Chinese)
[3]
VICENTE N M,ANGEL S A,ALVARO C.Model of the aerodynamic behavior of a pararotor[J].Journal of Aircraft,2006,43(6):1-15.
[4]
VICENTE N M,ANGEL S A,ALVARO C.Experimental investigation of an autorotating?wing aerodynamic decelerator system[C]//18th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar.Munich,Alemania:AIAA,2005:1-15.
[5]
VICENTE N M,PIECHOCKI J,CUERVA A,et al.Experimental research on a vertically falling rotating wing decelerator model[C]//19th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar.Williamsburg,VA:AIAA,2007:2 568-2 583.
HU Zhi?peng,LIU Rong?zhong,GUO Rui.Aerodynamic characteristics of two wings terminal sensitive projectile based on Fluent[J].Flight Dynamics,2013,31(1):53-60.(in Chinese)
HU Zhi?peng,LIU Rong?zhong,GUO Rui.Effect of two?typical wing shapes on aerodynamic characteristics of non?parachute terminal?sensitive projectile[J].Journal of Nanjing University of Science and Technology,2010,36(5):739-744.(in Chinese)
[10]
王爱中.无伞末敏弹稳态扫描特性研究[D].南京:南京理工大学,2008.
[11]
WANG Ai?zhong.Research on the stable scanning motion of the terminal?sensitive ammunition with two wing panels[D].Nanjing:Nanjing University of Science and Technology,2008.(in Chinese)
JIANG Li?ping,ZHANG Xu?chun,WANG Ping.Optimal design of system efficiency parameters about terminal sensitive projectiles based on support vector machine and genetic algorithm[J].Journal of Naval University of Engineering,2007,19(1):32-34.(in Chinese)
HUANG Feng?hua,LIU Rong?zhong,GUO Rui.Optimal design of system efficiency parameters about terminal?sensitive?projectiles based on hybrid neural network[J].Computer Simulation,2012,29(3):53-56.(in Chinese)
[17]
叶慈南,曹伟丽.应用数理统计[M].北京:机械工业出版社,2004:279-290.
[18]
YE Ci?nan,CAO Wei?li.Applied mathematical statistics[M].Beijing:China Machine Press,2004:279-290.(in Chinese)
[19]
GUO Rui,LIU Rong?zhong,WANG Ben?he,et al.Experimental study on decelerating and spinning characteristics of an asymmetric two?wing projectile[J].Journal of Projectiles,Rockets,Missiles and Guidance,2009,29(5):249-254.(in Chinese)
HUANG Kun,CHEN Sen?fa,LIU Rong?zhong.Optimal design of system efficiency parameters about terminal?sensitive?projectiles based on neural network and genetic algorithm[J].Acta Armamentarii,2004,25(3):257-260.(in Chinese)