[1] 张龙,赵志勤,范斌宁,等. 基于弹载地磁测试的高速旋转稳定弹锥形运动分析[J].兵工学报,2016,37(12):2235-2241. ZHANG Long, ZHAO Zhi-qin, FAN Bin-ning, et al. Analysis on coning motion of high-speed spin-stabilized projectile base on on-board magnetic test[J].Acta Armamentarii, 2016, 37(12): 2235- 2241. (in Chinese) [2] 杨树兴,赵良玉,闫晓勇. 旋转弹动态稳定性理论[M].北京:国防工业出版社,2014:1-27. YANG Shu-xing, ZHAO Liang-yu, YAN Xiao-yong. Dynamics stability of spinning missiles[M]. Beijing: National Defense Industry Press, 2014: 1-27. (in Chinese) [3] 闫晓勇,杨树兴,张成. 基于章动运动理论的火箭弹锥形运动稳定性分析[J].兵工学报,2009,30(10):1291-1296. YAN Xiao-yong, YANG Shu-xing, ZHANG Cheng. Analysis of stability for coning motion of rockets based on theory of nutation movement[J]. Acta Armamentarii, 2009, 30(10): 1291-1296. (in Chinese) [4] 崔垚,李顺利,计佳俊,等. 空空导弹高抛弹道作战效能研究[J].飞行力学,2012,30(4):376-384. CUI Yao, LI Shun-li, JI Jia-jun, et al. Study on the operational effectiveness of high parabola trajectory of air-to-air missile[J]. Flight Dynamics, 2012, 30(4): 376-384. (in Chinese) [5] Li M J, Rui X T, Abbas L K. Elastic dynamic effects on the trajectory of a flexible launch vehicle[J]. Journal of Spacecraft and Rockets, 2015, 52(6): 1586-1602. [6] Shi Z J, Zhao L Y. Effects of aeroelasticity on coning motion of a spinning missile[J]. Proceedings of the Institution of Mechanical Engineers Part G: Journal of Aerospace Engineering, 2016, 230(14): 2581-2591. [7] 黄程德,郑冠男,杨国伟,等. 基于CFD/CSD耦合间隙三维全动舵面气动弹性研究[J].应用力学学报,2018,35(1):1-8. HUANG Cheng-de, ZHENG Guan-nan, YANG Guo-wei,et al. Aeroelastic study of a three dimensional all-movable wing with free play using CFD/CSD coupling[J]. Chinese Journal of Applied Mechanics, 2018, 35(1): 1-8. (in Chinese) [8] 郭东,徐敏,陈士橹. 弹性飞行器飞行动力学建模研究[J].空气动力学学报,2013,31(4):413-419. GUO Dong, XU Min, CHEN Shi-lu. Research on flight dynamic modeling of highly flexible aircrafts[J]. Acta Aerodynamica Sinica, 2013, 31(4): 413-419. (in Chinese) [9] Platus D H. Aeroelastic stability of slender, spinning missiles[J]. Journal of Guidance, Control and Dynamics, 1992, 15(1): 144-151.
[10] Murphy C H, Mermagen W H. Flight mechanics of an elastic symmetric missile[J]. Journal of Guidance, Control and Dyna- mics, 2001, 24(6): 1125-1132. [11] Canavin J R, Likins P W. Floating reference frames for flexible spacecraft[J]. Journal of Spacecraft, 1977, 14(12): 724-732. [12] 赵贺伟,杨秀霞,沈如松,等. 弹性高超声速飞行器预设性能精细姿态控制[J].兵工学报,2017,38(3):501-511. ZHAO He-wei, YANG Xiu-xia, SHEN Ru-song, et al. Prescribed performance fine attitude control for aeroelastic hypersonic vehicle[J]. Acta Armamentarii, 2017, 38(3): 501-511. (in Chinese) [13] 张希彬,宗群,曾凡琳. 考虑气动—推进—弹性耦合的高超声速飞行器面向控制建模与分析[J].宇航学报,2014,35(5):528-536. ZHANG Xi-bin, ZONG Qun, ZENG Fan-lin.Control-oriented modeling and analysis of a hypersonic vehicle with coupled aerodynamic-propulsion-elastic[J]. Journal of Astronautics, 2014, 35(5): 528-536. (in Chinese) [14] Waszak M R, Schmidt D K. Flight dynamics of aeroelastic vehicles[J]. Journal of Aircraft, 1988, 25(6): 563-571. [15] Xu T F, Rong J L, Xiang D L, et al. Dynamic modeling and stability analysis of a flexible spinning missile under thrust[J]. International Journal of Mechanical Sciences, 2016, 119: 144-154. [16] Zhang Z, Li S L. Two-degree controller design for flexible missile based on H-inf interference suppression[C]∥Proceedings of the 2nd International Conference on Instrumentation & Measurement, Computer, Communication and Control.Harbin, China: IEEE, 2012: 1653-1656. [17] 李惠峰. 高超声速飞行器制导与控制技术[M].北京:中国宇航出版社,2012:84-100. LI Hui-feng. Guidance and control technology of hypersonic vehicle[M]. Beijing: China Astronautic Publishing House, 2012: 84-100. (in Chinese) [18] Hu Q L, Meng Y, Wang C L, et al. Adaptive backstepping control for air-breathing hypersonic vehicles with input nonlinearities[J]. Aerospace Science and Technology, 2018, 73(2): 289-299. [19] Meirovitch L, Tuzcu I. The lure of the mean axis[J]. Journal of Applied Mechanics, 2007, 74(3): 497-504. [20] Meirovitch L, Tuzcu I. Unified theory for the dynamics and control of maneuvering flexible aircraft[J]. AIAA Journal, 2004, 42(4): 714-727.
第39卷 第11期2018 年11月兵工学报ACTA ARMAMENTARIIVol.39No.11Nov.2018
|