[1] Lei J M, Wu J S. Aerodynamic configuration design for extended range guided munition[J]. Acta Aeronautica et Astronautica Sinica, 2005, 26(3): 294-297 (in Chinese). 雷娟棉, 吴甲生. 增程制导炮弹气动外形设计[J]. 航空学报, 2005, 26(3): 294-297.
[2] Chen Q, Wang Z Y, Chang S J, et al. Optimal trajectory design under uncertainly for a gliding guided projectile[J].Acta Aeronautica et Astronautica Sinica, 2014, 35(9): 2593-2604 (in Chinese). 陈琦, 王中原, 常思江,等. 不确定飞行环境下的滑翔制导炮弹方案弹道优化[J]. 航空学报, 2014, 35(9): 2593-2604.
[3] Zhang M Q, Liu D F, Wang D M, et al. A summary for trajectory correction projectiles[J]. Acta Armamentarii, 2010, 32(2): 127-130 (in Chinese). 张民权, 刘东方, 王冬梅, 等. 弹道修正弹发展综述[J]. 兵工学报, 2010, 32(2): 127-130.
[4] Gagnon E, Lauzon M. Course correction fuze concept analysis for in-service 155 mm spin-stabilized gunnery projectiles[C]//AIAA Guidance, Navigation and Control Conference and Exhibit. Reston: AIAA, 2008: 1-20.
[5] Pettersson T, Buretta R, Cook D. Aerodynamics and flight stability for a course corrected artillery round[C]//Proceedings of the 23rd International Symposium on Ballistics. Tarragona, Spain: International Ballistics Committee, 2007: 647-653.
[6] Wang Z G, Li W, Zhang Z N. Dynamics modeling of guided dual-spin rocket[J]. Acta Armamentarii, 2013, 34(7): 910-915 (in Chinese). 王志刚, 李伟, 张振宁. 双旋制导火箭弹动力学建模[J]. 兵工学报, 2013, 34(7): 910-915.
[7] Reg F J, Smith J. Aeroballistics of a terminally corrected spinning projectile (TCSP)[J]. Journal of Spacecraft and Rockets, 1975, 12(12): 733-738.
[8] Costello M, Peterson A. Linear theory of a dual-spin projectile in atmospheric flight[J]. Journal of Guidance, Control, and Dynamics, 2000, 23(5): 789-797.
[9] Rogers J, Costello M. Design of a roll-stabilized mortar projectile with reciprocating canards[J]. Journal of Guidance, Control, and Dynamics, 2010, 33(4): 1026-1034.
[10] Theodoulis S, Gassmann V, Wernert P, et al. Guidance and control design for a class of spin-stabilized fin-controlled projectiles[J]. Journal of Guidance, Control, and Dynamics, 2013, 36(2): 517-531.
[11] Wernert P, Theodoulis S. Modelling and stability analysis of the 155 mm spin-stabilised projectile equipped with course correction fuse(CCF)[J]. International Journal of Modelling, Identification and Control, 2011, 14(3): 189-204.
[12] Theodoulis S, Wernert P. Flight control for a class of 155 mm spin-stabilized projectiles with course correction fuse (CCF)[C]//AIAA Guidance, Navigation and Control Conference. Reston: AIAA, 2011: 1-10.
[13] Wernert P. Stability analysis for canard guided dual-spin stabilized projetiles[C]//Proceedings of the AIAA Atmospheric Flight Mechanics Conference and Exhibit. Reston: AIAA, 2009: 1-24.
[14] Lloyd K H, Brown D P. Instability of spinning projectiles during terminal guidance[J]. Journal of Guidance, Control, and Dynamics, 1979, 2(1): 65-70.
[15] Cloutier G J. Stable rotation states of dual-spin spacecraft[J]. Journal of Spacecraft and Rockets, 1968, 5(4): 490-492.
[16] Likins P W. Attitude stability criteria for dual spin spacecraft[J]. Journal of Spacecraft and Rockets, 1967, 4(12): 1638-1643.
[17] Ji X L, Wang H P, Zeng S M, et al. CFD prediction of longitudinal aerodynamics for a spinning projectile with fixed canard[J]. Transactions of Beijing Institute of Technology, 2011, 31(3): 265-268 (in Chinese). 纪秀玲, 王海鹏, 曾时明, 等. 可旋转鸭舵对旋转弹丸纵向气动特性的影响[J]. 北京理工大学学报, 2011, 31(3): 265-268.
[18] Hao Y P, Meng Q Y, Zhang J Y. Aerodynamic characteristic analysis on two-dimensional trajectory corrector shell with fixed-wing[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2012, 32(3): 171-173 (in Chinese). 郝永平, 孟庆宇, 张嘉易. 固定翼二维弹道修正弹气动特性分析[J]. 弹箭与制导学报, 2012, 32(3): 171-173.
[19] Han Z P. Rocket exterior ballistics [M]. Beijing: Beijing Institute of Technology Press: 2008: 145-149 (in Chinese). 韩子鹏. 弹箭外弹道学[M]. 北京: 北京理工大学出版社, 2008: 145-149.
[20] Qian X F, Lin R X, Zhao Y N. Missile flight mechanics[M]. Beijing: Beijing Institute of Technology Press, 2008:53-55 (in Chinese). 钱杏芳, 林瑞雄, 赵亚男. 导弹飞行力学[M]. 北京: 北京理工大学出版社, 2008: 53-55.
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