[1] 徐国华, 史勇杰, 招启军, 等. 直升机旋翼气动噪声的研究新进展[J]. 航空学报, 2017, 38(7): 520991. XU G H, SHI Y J, ZHAO Q J, et al. New research progress in helicopter rotor aerodynamic noise[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(7): 520991 (in Chinese). [2] 向锦武, 郭俊贤, 张晓谷. 直升机减振的旋翼桨叶优化设计研究综述[J]. 北京航空航天大学学报, 2001, 27(1): 32-35. XIANG J W, GUO J X, ZHANG X G. An overview of rotor blades optimum design for helicopter vibration reduction[J]. Journal of Beijing University of Aeronautics and Astronautics, 2001, 27(1): 32-35 (in Chinese). [3] HAO Z Y, LI X, CAO X, et al. A cross-coupled control strategy of phase difference for electric vibration damping actuator[J]. IEEE Access, 2020, 8: 213887-213898. [4] 朱翔, 殷学吉, 李天匀, 等. 基于惯容器的动力反共振隔振器隔振特性分析[J]. 哈尔滨工程大学学报, 2016, 37(10): 1318-1322. ZHU X, YIN X J, LI T Y, et al. Analysis of the vibration isolation characteristics of dynamic anti-resonance isolators based on an inerter[J]. Journal of Harbin Engineering University, 2016, 37(10): 1318-1322 (in Chinese). [5] 庞俊恒. 基于压电元件的振动被动控制技术研究[D].南京:南京理工大学, 2004. PANG J H. Research on passive vibration control technology based on piezoelectric elements[D]. Nanjing: Nanjing University of Science and Technology, 2004(in Chinese). [6] 林长亮, 王金亮, 张亚军, 等. 直升机振动主动控制技术研究现状[C]//探索 创新 交流——第六届中国航空学会青年科技论坛文集(上册). 北京: 中国航空学会, 2014: 6. LIN C L, WANG J L, ZHANG Y J, et al. Research status of active helicopter vibration control technology[C]//Exploring and Innovating Exchange—Proceedings of the Sixth Chinese Society of Aeronautics and Astronautics (Volume 1). Beijing: Chinese Aeronautical Society, 2014: 6 (in Chinese). [7] GARNJOST K D, REY G J. Modular vibratory force generator, and method of operating same: US5903077[P]. 1999-05-11. [8] JUNG S U, KWAK D I, KIM S H, et al. Vibration reduction devices for Korean utility helicopter[J]. Journal of the Korean Society for Aeronautical & Space Sciences, 2013, 41(12): 987-993. [9] KIM D H, KIM T J, PAEK S K, et al. Application and performance evaluation of helicopter active vibration control system for surion[J]. Journal of the Korean Society for Aeronautical & Space Sciences, 2015, 43(6): 557-567. [10] JOLLY M R, ALTIERI R E, BADRE-ALAM A, et al. Helicopter vibration control system and circular force generation systems for canceling vibrations: US9776712[P]. 2017-10-03. [11] 李维嘉, 曹青松. 船舶振动主动控制的研究进展与评述[J]. 中国造船, 2007, 48(2): 68-79. LI W J, CAO Q S. Advances and review on the research of the active control of ship vibration[J]. Ship Building of China, 2007, 48(2): 68-79 (in Chinese). [12] 郝振洋, 王涛, 曹鑫, 等. 旋转偏心质量块式消振电力作动器建模与控制[J]. 振动工程学报, 2022, 35(1): 209-219. HAO Z Y, WANG T, CAO X, et al. Modeling and control of rotating eccentric mass block vibration damping electric actuator[J]. Journal of Vibration Engineering, 2022, 35(1): 209-219 (in Chinese). [13] 韩广才, 李鸿, 王芝秋.船舶电动消振作动器研究[J].哈尔滨工程大学学报, 2005(1): 39-43. HAN G C, LI H, WANG Z Q.Research on ship’s electric vibration damping actuator[J]. Journal of Harbin Engineering University, 2005(1): 39-43(in Chinese). [14] 宋来收,夏品奇.直升机振动主动控制的机身/压电叠层作动器耦合优化法[J].航空学报,2011,32(10):1835-1841. SONG L S, XIA P Q.The coupling optimization method of fuselage/piezoelectric laminated actuator for active control of helicopter vibration[J]. Acta Aeronautica Sinica,2011,32(10):1835-1841(in Chinese). [15] 汪文涛, 刘正江, 李新民. 用于离心式作动器的变滑模面滑模控制[J]. 航空学报, 2019, 40(12): 323210. WANG W T, LIU Z J, LI X M. Variable sliding mode sliding mode controller for centrifugal harmonic force generator[J]. Acta Aeronautica et Astronautica Sinica, 2019, 40(12): 323210 (in Chinese). [16] DINCEL E, SÖYLEMEZ M T. Limitations on domin ant pole pair selection with continuous PI and PID controllers[C]//2016 International Conference on Control,Decision and Information Technologies (CoDIT), 2016: 741-745. [17] 王鑫鑫. 基于热连轧机耦合振动的主动抑振控制研究[D]. 北京: 北京科技大学, 2019. WANG X X. Research on active vibration suppression control based on coupled vibration of hot strip mill[D]. Beijing: University of Science and Technology Beijing, 2019(in Chinese). [18] LEHTOMAKI N, SANDELL N, ATHANS M. Robustness results in linear-quadratic Gaussian based multivariable control designs[J]. IEEE Transactions on Automatic Control, 1981, 26(1): 75-93. [19] MUKHOPADHYAY V, NEWSOM J. Application of matrix singular value properties for evaluating gain and phase margins of multiloop systems[C]//Guidance and Control Conference. Reston: AIAA, 1982: 420-428. [20] 袁海宵, 王慧贞. 基于无刷直流电动机伺服系统的位置环设计[J]. 电力电子技术, 2011, 45(4): 52-54, 84. YUAN H X, WANG H Z. The design of digital three loops servo system based on brushless DC motor[J]. Power Electronics, 2011, 45(4): 52-54, 84 (in Chinese). [21] 李信栋, 苟兴宇. 多输入多输出线性定常系统稳定裕度的分析与改进[J]. 控制理论与应用, 2014, 31(1): 105-111. LI X D, GOU X Y. Analysis and improvement of stability margin for multi-input multi-output linear time-invariant systems[J]. Control Theory & Applications, 2014, 31(1): 105-111 (in Chinese). [22] 李信栋, 苟兴宇. 由回差阵奇异值求稳定裕度的退化算法[J]. 控制理论与应用, 2016, 33(4): 460-465. LI X D, GOU X Y. Degraded algorithm for determining stability margin by using singular value of the return difference matrix[J]. Control Theory & Applications, 2016, 33(4): 460-465 (in Chinese). |