[1] 杨树兴. 陆军多管火箭武器的发展与思考[J]. 兵工学报, 2016, 37(7): 1299-1305. YANG S X. Progress and key points for guidance of multiple launch rocket systems[J]. Acta Armamentarii, 2016, 37(7): 1299-1305. (in Chinese) [2] 陈成, 赵良玉, 谢浩怡, 等. 单通道控制旋转弹角运动的复分析方法[J]. 兵工学报, 2021, 42(2): 308-319. CHEN C, ZHAO L Y, XIE H Y, et al. Complex analysis for angular motion of a spinning projectile with one pair of canards[J]. Acta Armamentarii, 2021, 42(2):308-319. (in Chinese) [3] 雷娟棉, 张嘉炜, 谭朝明. 小攻角下船尾外形对旋转弹丸马格努斯效应影响的数值研究[J]. 兵工学报, 2017, 38(9): 1705-1714. LEI J M, ZHANG J W, TAN Z M. Influence of boattail on the Magnus effect of spinning non-finned projectile at small angles of attack[J]. Acta Armamentarii, 2017, 38(9): 1705-1714. (in Chinese) [4] 王波兰, 李克勇, 杨永强. 近程/末端旋转导弹发展及关键技术综述[J]. 上海航天, 2017, 34:1-6. WANG B L, LI K Y, YANG Y Q. Review of development and key techniques of rolling airframe missiles[J]. Aerospace Shanghai, 2017, 34: 1-6. (in Chinese) [5] 张平, 赵志明, 贾波, 等. 尾翼稳定火箭弹高原姿态运动规律研究[J]. 兵工学报, 2016, 37(8): 1345-1350. ZHANG P, ZHAO Z M, JIA B, et al. Research on attitude motion law of rockets on plateau[J]. Acta Armamentarii, 2016, 37(8): 1345-1350. (in Chinese) [6] 丁天宝, 何朝, 王良明, 等. 高速旋转炮弹宽海拔弹道解算方法[J]. 兵工学报, 2021, 42(1):209-213. DING T B, HE Z, WANG L M, et al. Calculation method of firing trajectory of high spinning projectile adapted to wide altitude[J]. Acta Armamentarii, 2021, 42(1): 209-213. (in Chinese) [7] 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. YANG S X, ZHAO L Y, YAN X Y. Dynamic stability of spinning missiles[M]. Beijing: National Defense Industry Press, 2014. (in Chinese) [8] IMBAULT J, TJULIN H, KINNEY R, et al. Mini-RIMS-a miniature roll-stabilized inertial measurement system[C]∥Proceedings of the 7th Conference on Sounding Rockets, Ballons and Related Space Systems. Ocean City, MD, US: AIAA, 1986:35-43. [9] YANG Z L, MO B, NIE Z. Design on MEMS Based Roll-Isolated SINS in Spinning Projectile[J]. Telecom Market, 2013(5): 46-51. [10] 李杰, 赵诣, 刘俊, 等. 高旋弹药飞行姿态测量用半捷联MEMS惯性测量装置研究[J]. 兵工学报, 2013, 34(11): 1398-1403. LI J, ZHAO Y, LIU J, et al. Research on semi-strapdown MEMS inertial measurement device for flight attitude measurement of high-speed rotating ammunition[J]. Acta Armamentarii, 2013, 34(11): 1398-1403. (in Chinese) [11] 李杰, 刘俊. 旋转弹用半捷联惯性测量系统数据传输技术[J]. 弹箭与制导学报, 2014, 34(4): 57-60. LI J, LIU J. Research on data transmission technology for rotating ammunition with semi-strapdown inertial measurement system[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2014, 34(4): 57-60. (in Chinese) [12] 周琪, 秦永元, 赵长山. 旋转弹用横滚隔离捷联惯导稳定回路设计[J]. 中国惯性技术学报, 2009, 17(4): 383-387. ZHOU Q, QIN Y Y, ZHAO C S. Design on stabilization loop of roll-isolated SINS in spinning projectile[J]. Journal of Chinese Inertial Technology, 2009, 17(4): 383-387. (in Chinese) [13] 周琪, 秦永元, 杨鹏翔. 横滚隔离激光捷联惯导系统稳定回路自抗扰控制[J]. 测控技术, 2009, 28(11): 95-100. ZHOU Q, QIN Y Y, YANG P X. Active disturbance rejection control of the stabilizing loop for roll-isolated laser gyro strapdown inertial navigation system[J]. Measurement & Control Technology, 2009, 28(11): 95-100. (in Chinese) [14] SHI Y S, WANG B, DONG M J, et al. Research of Roll-Isolated Gimbal Platform and a Two-Position Initial Alignment Scheme of SINS in Spinning Projectile[J]. Advanced Materials Research, 2012, 383-390: 4115-4120. [15] 刘一鸣, 李杰, 王一焕, 等. 旋转弹用轴向减旋平台控制系统设计[J]. 电子器件, 2017, 40(4): 965-972. LIU Y M, LI J, WANG Y H, et al. Design of the control system for axial anti-rotation platform used in rotating ammunition[J]. Chinese Journal of Electron Devices, 2017, 40(4): 965-972. (in Chinese) [16] SONG J C, YANG S X, XIONG F F. Control failure of the roll-isolated inertial navigation system under large pitch angle[J]. Chinese Journal of Aeronautics, 2020, 33(10): 2707-2715. [17] 朱爱华, 朱成九, 张卫华. 滚动轴承摩擦力矩的计算分析[J]. 轴承, 2008(7): 1-3. ZHU A H, ZHU C J, ZHANG W H. Analysis on calculation of friction torque of rolling bearings[J]. Bearing, 2008(7): 1-3. (in Chinese) [18] 韩京清, 王伟. 非线性跟踪-微分器[J]. 系统科学与数学, 1994, 14(3): 177-183. HAN J Q, WANG W. Nonlinear tracking-differentiator[J]. Journal of Systems Science and Mathematical Sciences, 1994, 14(3): 177-183. (in Chinese) [19] 韩京清. 自抗扰技术:估计补偿不确定因素的控制技术[M]. 北京: 国防工业出版社, 2008. HAN J Q. Active disturbance rejection control technique-the technique for estimating and compensating the uncertainties[M]. Beijing: National Defense Industry Press, 2008. (in Chinese) [20] 赵春哲, 黄以. 基于自抗扰控制的制导与运动控制一体化设计[J]. 系统科学与数学, 2010, 30(6): 742-751. ZHAO C Z, HUANG Y. ADRC based integrated guidance and control scheme[J]. Journal of Systems Science and Mathematical Sciences, 2010, 30(6): 742-751. (in Chinese) [21] 唐彬彬, 徐道明, 吴若鸷. 永磁同步电机自抗扰控制调速系统[J]. 电机与控制应用, 2020, 47(3):12-16. TANG B B, XU D M, WU R Z. Active disturbance rejection control speed regulation system for PMSM[J]. Electric Machines & Control Application, 2020, 47(3): 12-16. (in Chinese) [22] 岳彬, 马文, 呼卫军. 高超声速飞行器的自适应容错控制[J]. 兵工学报, 2021, 42(3): 521-529. YUE B, MA W, HU W J. Adaptive fault-tolerant control of hypersonic vehicles[J]. Acta Armamentarii, 2021, 42(3): 521-529. (in Chinese) [23] 韦常柱, 琚啸哲, 徐大富, 等. 垂直起降重复使用运载器返回制导与控制[J]. 航空学报, 2019, 40(7): 322782. WEI C Z, JU X Z, XU D F, et al. Guidance and control for return process of vertical takeoff vertical landing reusable launching vehicle[J]. Acta Aeronautica et Astronautica Sinica, 2019, 40(7): 322782. (in Chinese) [24] 张茜丹, 尹达一. 自抗扰控制器在高阶系统中仿真实现[J]. 航天控制, 2018, 36(1): 3-13. ZHANG X D, YIN D Y. Simulation study of active disturbance rejection controller for high order systems[J]. Aerospace Control, 2018, 36(10): 3-13. (in Chinese)
|