赵宏斌.直接力/气动力复合控制的导弹伺服弹性分析[D].哈尔滨:哈尔滨工业大学控制与仿真中心, 2010 Zhao Hongbin.Servo elastic analysis on missile with lateral jets and aerodynamics control[D].Harbin:Harbin Institute of Technology Control and Simulation Center, 2010 (in Chinese)
[2]
Rick L, James R B, Andrew K S.Multi-loop aeroservoelastic control of a hypersonic vehicle.AIAA-1999-4123, 1999
[3]
姜玉宪, 李行善, 吴明玉, 等.飞行器结构振动和控制系统解耦及主动抑制的研究[J].宇航学报, 1985 (2):78-87 Jia Yuxian, Li Xingshan, Wu Mingyu, et al.A study of active vehicle structure vibration and decoupling with control system as well as initiative suppression[J].Journal of Astronautics, 1985 (2):78-87 (in Chinese)
[4]
Cheng M H, Tsai J L.A new ⅡR adaptive notch filter[J].Signal Processing, 2006, 86:1648-1655
[5]
江清潘, 常太华, 朱红路, 等.自适应噪声消除算法的性能比较与仿真[J].科学技术与工程, 2009, 19 (9):5836-5838 Jiang Qingpan, Chang Taihua, Zhu Honglu, et al.Performance comparisons and simulations of adaptive noise cancellation algorithms[J].Science Technology and Engineering, 2009, 19 (9):5836-5838 (in Chinese)
[6]
Paul J K, Douglas G M.Adaptive spatial filtering for aeroservoelastic response suppression.AIAA-2009-5709, 2009
[7]
朱敬举, 王军素.导弹控制系统设计中的弹体弹性振动问题及陷波滤波器设计[J].邢台职业技术学院学报, 2005, 22 (5):1-4 Zhu Jinju, Wang Junsu.Method for the design of notch filter and the problem of elastic vibration of missile body-s control system[J].Journal of Xingtai Polytechnic College, 2005, 22 (5):1-4 (in Chinese)
[8]
张雷, 彭程, 王永, 等.大长径比导弹两自由度H∞减振跟踪控制器设计[J].弹道学报, 2010, 22 (4):1-5 Zhang Lei, Peng Cheng, Wang Yong, et al.Two-degree-of-freedom H∞ controller design for vibration attenuation and tracking of high length-to-diameter ratio missile[J].Journal of Ballistics, 2010, 22 (4):1-5 (in Chinese)
[9]
陈文俊.国外飞行器气动伺服弹性研究概况[J].飞航导弹, 2000 (7):36-41 Chen Wenjun.Foreign aircraft aeroservoelastic study overview[J].Winged Missiles Journal, 2000 (7):36-41 (in Chinese)
[10]
Oh Choong, Bang Hyochoong, Park Chang-Su.Attitude control of a flexible launch vehicle using an adaptive notch filter:ground experiment[J].Control Engineering Practice, 2008, 16 (1):30-42
[11]
陈晓曾, 陈勇.一种用于主动噪声抑制系统的次级通道特性识别算法的改进[J].噪声与振动控制, 2003 (6):21-24 Chen Xiaozeng, Chen Yong.An improved secondary path modeling algorithm for active noise control system[J].Noise and Vibration Control, 2003 (6):21-24 (in Chinese)
[12]
郑勇斌, 林丽.采用摆动喷管推力矢量控制弹性弹体数学模型建立[J].现代防御技术, 2007, 35 (1):41-44 Zheng Yongbin, Lin Li.Mathematical model of elasticity missiles with swing nozzle thrust vector control[J].Modern Defence Technology, 2007, 35 (1):41-44 (in Chinese)
楚龙飞, 吴志刚, 杨超, 等.导弹自适应结构滤波器的设计与仿真[J].航空学报, 2011, 32 (2):195-201 Chu Longfei, Wu Zhigang, Yang Chao, et al.Design and simulation of adaptive structure-filter for missiles[J].Modern Acta Aeronautica et Astronautica Sinica, 2011, 32 (2):195-201 (in Chinese)
[15]
Rick L, James R B, Andrew K S.Multi-loop aeroservoelastic control of a hypersonic vehicle.AIAA-1999-4123, 1999
[16]
Cheng M H, Tsai J L.A new ⅡR adaptive notch filter[J].Signal Processing, 2006, 86:1648-1655
[17]
江清潘, 常太华, 朱红路, 等.自适应噪声消除算法的性能比较与仿真[J].科学技术与工程, 2009, 19 (9):5836-5838 Jiang Qingpan, Chang Taihua, Zhu Honglu, et al.Performance comparisons and simulations of adaptive noise cancellation algorithms[J].Science Technology and Engineering, 2009, 19 (9):5836-5838 (in Chinese)
[18]
Paul J K, Douglas G M.Adaptive spatial filtering for aeroservoelastic response suppression.AIAA-2009-5709, 2009
[19]
朱敬举, 王军素.导弹控制系统设计中的弹体弹性振动问题及陷波滤波器设计[J].邢台职业技术学院学报, 2005, 22 (5):1-4 Zhu Jinju, Wang Junsu.Method for the design of notch filter and the problem of elastic vibration of missile body-s control system[J].Journal of Xingtai Polytechnic College, 2005, 22 (5):1-4 (in Chinese)
