李晓晖 , 惠钰 , 郑佩 , 杨军 . 鸭式布局火箭滚转特性试验研究[J]. 弹箭与制导学报, 2023 , 43(1) : 111 -116 . DOI: 10.15892/j.cnki.djzdxb.2023.01.016

[1]	张晓旻, 程养民, 李怀念, 等. 自由滚转尾翼试飞器滚转特性分析[J]. 固体火箭技术, 2008, 31(4): 307-309. ZHANG X M, CHENG Y M, LI H N, et al. Analysis on rolling characteristics of test flight vehicle with free-rolling tail[J]. Journal of Solid Rocket Technology, 2008, 31(4): 307-309.

[2]	张龙, 吴小役, 刘芳, 等. 简易制导弹滚转控制研究[J]. 四川兵工学报, 2011, 32(2): 38-41. ZHANG L, WU X Y, LIU F, et al. Study on the rolling control of simple guided missile[J]. Journal of Sichuan Ordnance, 2011, 32(2): 38-41.

[3]	吴军飞, 田小虎, 童木华, 等. 鸭式布局导弹滚转控制时的侧向气动特性[J]. 弹道学报, 2013, 25(4): 11-14. WU J F, TIAN X H, TONG M H, et al. Lateral aerodynamic characteristics of canard-configuration missile under rolling control[J]. Journal of Ballistics, 2013, 25(4): 11-14.

[4]	曾广存, 丁庆国, 秦伊贤, 等. 鸭式布局导弹滚动气动控制方案及力矩分析[J]. 空气动力学学报, 1988, 6(3): 376-381. ZENG G C, DING Q G, QIN Y X, et al. A method to control rolling characteristics of canard missiles and an analysis of rolling moments[J]. ACTA Aerodynamica Sinica, 1988, 6(3): 376-381.

[5]	纪楚群. 导弹空气动力学[M]. 北京: 宇航出版社, 1996. JI C Q. Aerodynamics of missile[M]. Beijing: China Astronautic Publishing House, 1996.

[6]	敬代勇. 鸭式导弹横滚气动特性研究[D]. 上海: 上海交通大学, 2012. JING D Y. The research on rolling characteristics of canard-controlled missiles[D]. Shanghai: Shanghai Jiao Tong University, 2012.

[7]	薛明. 鸭式布局火箭弹鸭舵下洗影响滚转气动特性研究[D]. 南京: 南京理工大学, 2015. XUE M. Aerodynamics analysis on effects of downwash induced by canard on roll control of the rocket with canard configuration[D]. Nanjing: Nanjing University of Science & Technology, 2015.

[8]	李克勇, 王建. 一种高机动鸭式布局导弹的转速控制方法研究[J]. 上海航天, 2017, 34(增刊1): 95-99. LI K Y, WANG J. Rolling rate control of high maneuvering rolling air-frame missile with canard configuration[J]. Aerospace Shanghai, 2017, 34(S1): 95-99.

[9]	党建涛, 封锋, 邹延兵. 简控火箭弹舵翼气动干扰特性研究[J]. 弹道学报, 2019, 31(1): 36-42. DOI DANG J T, FENG F, ZOU Y B. Aerodynamic interference characteristics between rudder and fin for simple control rocket with fixed canard rudder[J]. Journal of Ballistics, 2019, 31(1): 36-42.

[10]	邢琳琳, 陈少松. 远程弹滚转特性研究综述[J]. 桂林航天工业高等专科学校学报, 2008, 13(1): 1-2. XING L L, CHEN S S. Overview of research on rolling characteristics of long range missiles[J]. Journal of Guiling College of Aerospace Technology, 2008, 13(1): 1-2.

[11]	郭向向, 曹红松, 程登华, 等. 鸭舵后掠角对火箭弹尾翼的滚转性能研究[J]. 弹箭与制导学报, 2017, 37(2): 170-172. Guo X X, CAO H S, CHENG D H, et al. Research of rolling characteristics on rocket wing by canard sweepback[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2017, 37(2): 170-172.

[12]	李克勇, 杨永强, 黄金. 高机动旋转导弹鸭式双通道控制研究[J]. 上海航天, 2016, 33(2): 53-57. LI K Y, YANG Y Q, HUANG J. Dual-channel canard control of spinning missile with high maneuvering[J]. Aerospace Shanghai, 2016, 33(2): 53-57.

[13]	李广超, 王得强, 高太元, 等. 高超声速翼舵干扰气动特性研究综述[J]. 飞航导弹, 2016(9): 21-27. LI G C, WANG D Q, GAO T Y. Overview of research on hypersonic aerodynamic characteristic of interference between wing and rudder[J]. Aerodynamic Missiles Journal, 2016(9): 21-27.

[14]	薛明, 陈少松, 倪金付. 鸭舵位置参数对弹箭滚转特性的影响[J]. 弹道学报, 2015, 27(2): 34-38. XUE M, CHEN S S, NI J F. Effects of canard position roll characteristics of canard control projectile[J]. Journal of Ballistics, 2015, 27(2): 34-38.

[15]	杜学伟. 弹箭双鸭舵滚转控制气动特性研究[D]. 南京: 南京理工大学, 2015. DU X W. Aerodynamic analysis on rolling controlling flight of close-coupled double-canard configuration missiles[D]. Nanjing: Nanjing University of Science & Technology, 2015.

[16]	敬代勇, 李剑. 鸭式与正常式导弹滚转特性数值研究[J]. 弹箭与制导学报, 2013, 33(4): 53-54. JING D Y, LI J. Numerical simulation of rolling characteristics on canard control missile and tail control missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2013, 33(4): 53-54.