[1] ROSERO J A, ORTEGA J A, ALDABAS E, et al. Moving towards a more electric aircraft[J]. IEEE Aerospace and Electronic Systems Magazine, 2007, 22(3):3-9.
[2] GARCIA A, CUISDO J, ROSERO J A, et al. Reliable electro-mechanical actuators in aircraft[J]. IEEE Aerospace and Electronic Systems Magazine, 2008, 23(8):19-25.
[3] 王娜, 周元钧. 基于负阻抗补偿法的调速系统阻抗特性分析[J]. 中国电机工程学报, 2013, 33(33):50-56. WANG N, ZHOU Y J. Impendance characteristics analysis of speed regulation system with negative input-resistance compensators[J]. Proceedings of the CSEE, 2013, 33(33):50-56(in Chinese).
[4] 吕宏, 袁海文, 张莉, 等. 基于模式重要度的航空电源系统可靠性估计[J]. 航空学报, 2010, 31(3):608-613. LU H, YUAN H W, ZHANG L, et al. Aircraft electrical power system reliability estimation based on pattern importance[J]. Acta Aeronautica et Astronautica Sinica, 2010, 31(3):608-613(in Chinese).
[5] MARIO R, ATEPHEN J. Aircraft electrical system architectures to support more electric aircraft[C]//Avionic & Systems Conference, 2004:27-35.
[6] JOSEPH A, WEIMER J A. Electrical power technology for the more electric aircraft[C]//IEEE/AIAA 12th DASC. Reston:AIAA, 1993:445-450.
[7] ARRILLAGA J, MEDINA A. The harmonic domain:A frame of reference for power system harmonic analysis[J]. IEEE Transactions on Power Systems, 1995, 10(1):433-440.
[8] 陈坚. 电力电子学[M]. 北京:高等教育出版社, 2010:194-199. CHEN J. Power electronics[M]. Beijing:Higher Education Press, 2010:194-199(in Chinese).
[9] 张崇巍, 张兴. PWM整流器及其控制[M]. 北京:机械工业出版社, 2003:69-78. ZHANG C W, ZHANG X. PWM rectifier and its control method[M]. Beijing:China Machine Press, 2003:69-78(in Chinese).
[10] 张巍, 尚晓磊, 周元钧, 等. 一种适用于航空电力作动器负载的三相PWM整流器最大功率控制[J]. 电工技术学报, 2011, 26(8):91-98. ZHANG W, SHANG X L, ZHOU Y J, et al. A maximum power control method of three-phase voltage source rectifiers adapted to aircraft electric actuator load[J]. Transactions of China Electrotechnical Society, 2011, 26(8):91-98(in Chinese).
[11] 王兆安, 杨军, 刘进军, 等. 谐波抑制与无功功率补偿[M]. 北京:机械工业出版社, 2005:257-321. WANG Z A, YANG J, LIU J J, et al. Harmonic suppression and reactive power compensation[M]. Beijing:China Machine Press, 2005:257-321(in Chinese).
[12] 张方华, 王明, 马义林, 等. 输入电压不平衡时的12脉冲自耦变压整流器[J]. 航空学报, 2010, 31(4):762-769. ZHANG F H, WANG M, MA Y L, et al. 12-pulse auto transformer rectifier unit under input voltage unbalance[J]. Acta Aeronautica et Astronautica Sinica, 2010, 31(4):762-769(in Chinese).
[13] CARLOS H I F, IVO B. A new high power factor bidirectional hybrid three-phase rectifier[C]//IEEE Applied Power Electronics Conference and Exposition. Piscataway, NJ:IEEE Press, 2006:1300-1306.
[14] RICARDO L A, IVO B. Analysis and implementation of a hybrid high power factor three phase unidirectional rectifier[J]. IEEE Transactions on Power Electronics, 2009, 24(3):632-640.
[15] ZHANG W, HOU Y Z, LIU X B, et al. Switched control of three-phase voltage source PWM rectifier under a wide-range rapidly varying active load[J]. IEEE Transactions on Power Electronics, 2012, 27(2):881-890.
[16] 杨培志, 张晓华, 陈宏钧, 等. 三相电压型PWM整流器模型准线性化[J]. 电工技术学报, 2007, 22(8):28-36. YANG P Z, ZHANG X H, CHEN H J, et al. Study of model quasi-linearization of three-phase voltage-type PWM rectifiers[J]. Transactions of China Electrotechnical Society, 2007, 22(8):28-36(in Chinese).
[17] 郑大钟. 线性系统理论[M]. 北京:清华大学出版社, 2011:305-334. ZHENG D Z. Linear system theory[M]. Beijing:Tsinghua University Press, 2011:305-334(in Chinese).
[18] 张锋. 线性二次型最优控制问题的研究[D]. 天津:天津大学, 2009:9-15. ZHANG F. Research on the problem of linear quadratic optimal control[D]. Tianjin:Tianjin University, 2009:9-15(in Chinese).
[19] KHAJEHODDIN S A, GHARTEMAN M K, BAKHSHAI A, et al. High quality output current control for single phase grid-connected inverters[C]//IEEE Applied Power Electronics Conference and Exposition. Piscataway, NJ:IEEE Press, 2014:1807-1814.
[20] 王娜, 周元钧. 负阻抗补偿法在机电作动器上的研究与应用[J]. 电机与控制学报, 2014, 18(4):25-30. WANG N, ZHOU Y J. Research and application on the negative input-resistance compensator for aircraft electromechanical actuator[J]. Electric Machines and Control, 2014, 18(4):25-30(in Chinese).
[21] WEIMER J A. Electrical power technology for the more electric aircraft[C]//IEEE/AIAA 12th Digital Avionics Systems Conference. Piscataway, NJ:IEEE Press, 1993:445-450. |