[1] 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, 31(增刊2): 127-130. ZHANG M Q, LIU D F, WANG D M, et al. A summary for trajectory correction projectiles[J]. Acta Armamentarii, 2010, 31(S2): 127-130. (in Chinese) [2] 许诺. 弹道修正弹动力学分析与控制方法研究[D]. 北京: 北京理工大学, 2015: 6-8. XU N. Research on dynamics analysis and control methods of trajectory correction projectiles[D]. Beijing: Beijing Institute of Technology, 2015: 6-8. (in Chinese) [3] GUO Q W, SONG W D, WANG Y, et al. Guidance law design for a class of dual-spin mortars[J]. International Journal of Aerospace Engineering, 2015,2015:952076. [4] WANG Y, SONG W D, FANG D, et al. Guidance and control design for a class of spin-stabilized projectiles with a two-dimensional trajectory correction fuze[J]. International Journal of Aerospace Engineering, 2015,2015:908304. [5] 张冬旭. 可控滚转二维弹道修正机构的研究[D]. 北京: 北京理工大学, 2015: 19-39. ZHANG D X. Research on rolling controlled two dimensional trajectory correction mechanism[D]. Beijing: Beijing Institute of Technology, 2015: 19-39. (in Chinese) [6] 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. [7] WERNERT P, LEOPOLD F, LEHMANN L. Wind tunnel tests and open-loop trajectory simulations for a 155 mm canards guided spin stabilized projectile [C]∥Proceedings of AIAA Atmospheric Flight Mechanics Conference and Exhibit. Reston, VA, US: AIAA, 2008. [8] WERNERT P. Stability analysis for canard guided dual-spin stabilized projectiles [C]∥Proceedings of AIAA Atmospheric Flight Mechanics Conference and Exhibit. Chicago, IL, US: AIAA, 2009. [9] SVE F, THEODOULIS S, WERNERT P, et al. Flight dynamics modeling of dual-spin guided projectiles[J]. IEEE Transactions on Aerospace and Electronic Systems, 2017, 53(4): 1625-1641.
[10] THEODOULIS S, WERNERT P. Flight dynamics & control for smart munition: the ISL contribution[J]. IFAC-PapersOnLine, 2017, 50(1): 15512-15517. [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 Z G, LI W, ZHANG Z N.Dynamics modeling of guided dual-spin rocket[J]. Acta Armamentarii, 2013, 34(7): 910-915. (in Chinese) [12] 许诺, 于剑桥, 王亚飞, 等. 固定翼双旋弹动力学特性分析[J]. 兵工学报, 2015, 36(4): 602-609. XU N, YU J Q, WANG Y F, et al.Analysis of dynamic characteristics of fixed-wing dual-spin projectiles[J]. Acta Armamentarii, 2015, 36(4): 602-609. (in Chinese) [13] 许诺, 于剑桥, 王亚飞. 固定翼双旋弹动力学分岔特性分析[J]. 航空学报, 2015, 36(12):3798-3808. XU N, YU J Q,WANG Y F. Dynamic bifurcation characteristics analysis on fixed-canard dual-spin projectiles[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(12): 3798-3808.(in Chinese) [14] 许诺, 于剑桥, 王亚飞. 基于周期平均的固定翼双旋弹弹道修正方法[J]. 航空学报, 2016, 36(9): 2892-2899. XU N, YU J Q, WANG Y F.Trajectory correcting method of fixed-canard of dual-spin projectiles based on period average[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(9): 2892-2899. (in Chinese) [15] 郭致远, 姚晓先, 张鑫. 基于周期平均的固定舵双旋火箭弹控制方法[J]. 航空学报, 2017, 38(12): 321307. GUO Z Y, YAO X X, ZHANG X.Trajectory correcting method of fixed-canard of dual-spin projectiles based on period average[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(12): 321307.(in Chinese) [16] 王钰, 王晓鸣, 程杰, 等.基于等效力方法的双旋弹侧向控制力落点响应分析[J]. 兵工学报, 2016, 37(8): 1379-1387. WANG Y, WANG X M, CHENG J, et al.Analysis on impact point response of dual-spin projectile with lateral force based on equivalent force method[J]. Acta Armamentarii, 2016, 37(8): 1379-1387.(in Chinese) [17] 常思江, 王中原, 刘铁铮. 鸭式布局双旋稳定弹强迫运动理论研究[J]. 兵工学报, 2016, 37(5): 829-839. CHANG S J, WANG Z Y, LIU T Z. A theoretical study of forced motion for dual-spin-stabilized projectiles with canards[J]. Acta Armamentarii, 2016, 37(5): 829-839.(in Chinese) [18] CHANG S J. Dynamic response to canard control and gravity for a dual-spin projectile[J]. Journal of Spacecraft and Rockets, 2016, 53(3): 558-566. [19] CHANG S J, WANG Z Y. Analysis of spin-rate property for dual-spin-stabilized projectiles with canards[J]. Journal of Spacecraft and Rockets, 2014, 51(3): 958-966. [20] LIU X D, LI D G, SHEN Q. Swerving orientation of spin-stabilized projectile for fixed-cant canard control input[J]. Mathema- tical Problems in Engineering, 2015, 2015: 173571. [21] WERNERT P, THEODOULIS S. Modeling and stability analysis for a class of 155 mm spin-stabilized projectiles with course correction fuse(CCF) [C]∥Proceedings of AIAA Atmospheric Flight Mechanics Conference and Exhibit. Portland, OR, US: AIAA, 2011. [22] ZHU D, TANG S, GUO J, et al. Flight stability of a dual-spin projectile with canards[J]. Proceedings of the Institute of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2015, 229(4):703-716. [23] BOYD S, EL-GHAOUI L, FERON E, et al. Linear matrix inequalities in system and control theory[M]. Philadelphia, PA, US: Society for Industrial and Mathematics, 1994:7-8. [24] SCHERER, C W. The Riccati inequality and state-space H∞-optimal control[D]. Würzburg, Germany:University of Würzburg, 1990:84-86. [25] RABINOWITZ S. How to find the square root of a complex number[J]. Mathematics and Informatics Quarterly,1993(3):54-56.
第40卷 第10期2019 年10月兵工学报ACTA ARMAMENTARIIVol.40No.10Oct.2019
|