[1] Bybee T. Precision guidance kit[C]∥45th Annual NDIA Gun and Missile Systems Conference. Dallas,TX: NDIA, 2010. [2] 郑斌, 王磊, 沈卫, 等. 世界兵器发展年度报告[R]. 北京:中国兵器工业集团公司第210研究所, 2012. ZHENG Bin, WANG Lei, SHEN Wei, et al. The annual report of world ordnance development[R]. Beijing: 210th Institute, China North Industries Group Corporation, 2012. (in Chinese) [3] 程杰, 于纪言, 王晓鸣, 等. 隔转鸭舵式弹道修正弹电磁执行机构工况研究[J]. 兵工学报, 2014, 35(12):2010-2015. CHENG Jie, YU Ji-yan, WANG Xiao-ming, et al. Research on working condition of electromagnetic actuator of trajectory correction projectile with decoupled canards[J]. Acta Armamentarii, 2014, 35(12):2010-2015.(in Chinese) [4] Regan F, Smith J. Aeroballistics of a terminally corrected spinning projectile[J]. Journal of Spacecraft and Rockets, 1975, 12(12):733-738. [5] Jermey C. Wind tunnel of a spinning 105 mm artillery shell model with control surfaces[R]. South Australia: Defense Science and Technology Organization, 1979. [6] Costello M F, Peterson A A. Linear theory of a dual-spin projectile at atmospheric flight[J]. Journal of Guidance, Control, and Dynamics, 2000, 23(5):789-797. [7] 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, 2010, 31(3):265-268. JI Xiu-ling, WANG Hai-peng, ZENG Shi-ming, et al. CFD prediction of longitudinal aerodynamics for a spinning projectile with fixed canards[J]. Transactions of Beijing Institute of Technology. 2010, 31(3): 265-268. (in Chinese) [8] 程杰,王晓鸣,于纪言,等. 次口径非对称鸭舵对弹道修正弹气动特性的影响[J]. 北京理工大学学报, 2015, 35(2): 133-138. CHENG Jie, WANG Xiao-ming, YU Ji-yan, et al. Study on the efect of sub-caliber asymmetry canards on the aerodynamics of trajectory correction projectiles [J]. Transactions of Beijing Institute of Technology, 2015, 35(2): 133-138.(in Chinese) [9] Je S E, Jung H S, Park M S, et al. A study on the aerodynamic characteristics for a spin-stabilized projectile with PGK[C]∥26th International Symposium on Ballistics. Miami:IBS, 2011. [10] Sahu J, Costello M, Montalvo C. Development and application of multidisciplinary coupled computational techniques for projectile aerodynamics[C]∥7th International Conference on Computational Fluid Dynamics. Hawaii:AIAA, 2012. [11] 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. WANG Zhi-gang, LI Wei, ZHANG Zhen-ning. Dynamics modeling of guided dual-spin rocket[J]. Acta Armamentarii, 2013, 34(7): 910-915.(in Chinese) [12] 程杰, 于纪言, 王晓鸣, 等. 隔转鸭舵式弹道修正弹气动力工程模型与辨识[J]. 兵工学报, 2014, 35(10):1542-1548. CHENG Jie, YU Ji-yan, WANG Xiao-ming, et al. Engineering modeling and identification of aerodynamics of trajectory correction projectile with decoupled canards[J]. Acta Armamentarii, 2014, 35(10):1542-1548.(in Chinese) [13] Da Ronch A, Vallespin D, Ghoreyshi M, et al. Computation of dynamic derivatives using CFD[C]∥28th AIAA Applied Aerodynamics Conference. Chicago, Illinois, US: AIAA, 2010. [14] Pattinson J, Lowenberg M H, Goman M G. Multi-degree-of-freedom wind-tunnel maneuver rig for dynamic simulation and aerodynamic model identification [J]. Journal of Aircraft, 2013, 50(2): 551-566. |