[1] 余远金.全主动磁悬浮飞轮转轴偏转控制方法及实验研究[D].北京:北京航空航天大学,2015.YU Y J.Study on the control method and experiment of the shaft tilting for the fully active magnetically suspended flywheel[D].Beijing:Beihang University,2015(in Chinese).
[2] FANG J C,ZHENG S Q,HANG B C.AMB vibration control for structural resonance of double-gimbal control moment gyro with high-speed magnetically suspended rotor[J].IEEE Transactions on Mechatronics,2013,18(1):32-43.
[3] REN Y,FANG J C.Current-sensing resistor design to include current derivative in PWM H-bridge unipolar switching power amplifiers for magnetic bearings[J].IEEE Transactions on Industrial Electronics,2012,59(12):4590-4600.
[4] 解永春.磁悬浮动量轮的主动振动控制[J].航天控制,2001(2):1-6.XIE Y C.Active vibration suppression for magnetically suspended momentum wheels[J].Aerospace Control,2001(2):1-6(in Chinese).
[5] 刘侃.动量矩可偏置磁悬浮动量轮结构设计[D].长沙:国防科学技术大学,2005.LIU K.The structure design of magnetic suspension momentum wheel with deflection angular momentum[D].Changsha:National University of Defense Technology,2005(in Chinese).
[6] 房建成,孙津济,樊亚洪.磁悬浮惯性动量轮技术[M].北京:国防工业出版社,2012:9-10.FANG J C,SUN J J,FAN Y H.Magnetically suspended inertial momentum wheel technology[M].Beijing:National Defense Industry Press,2012:9-10(in Chinese).
[7] BICHLER U,ECKARDT T.A gimbaled low noise momentum wheel[C]//27th Aerospace Mechanisms Symposium.1993,1:181-196.
[8] SAWADA H,HASHIMOTO T,NINOMIYA K.High-stability attitude control of satellites by magnetic bearing wheels[J].Transaction of the Japan Society for Aeronautical and Space Science,2001,44(145):133-141.
[9] ROSSINI L,CHETELAT O,ONILLON E,et al.Force and torque analytical models of a reaction sphere actuator based on spherical harmonic rotation and decomposition[J].IEEE/ASME Transactions on Mechatronics,2013,18(3):1006-1018.
[10] SEDDON J,PECHEV A.3-D wheel:A single actuator providing three-axis control of satellites[J].Journal of Spacecraft and Rockets,2012,49(3):553-556.
[11] 王春娥.惯性执行机构用高承载比低功耗磁轴承设计方法与实验研究[D].北京:北京航空航天大学,2014.WANG C E.Design method and experimental research on high specific load capacity and low loss magnetic bearing in inertia actuator[D].Beijing:Beihang University,2014(in Chinese).
[12] JASTRZE BSKI R P,PÖLLÄNEN R.Compensation of nonlinearities in active magnetic bearings with variable force bias for zero- and reduced-bias operation[J].Mechatronics,2009,19(5):629-638.
[13] HAN F T,GAO Z Y,LI D M,et al.Nonlinear compensation of active electrostatic bearings supporting a spherical rotor[J].Sensors and Actuators A:Physical,2005,119(1):177-186.
[14] CHEN M,KNOSPE C.Feedback linearization of active magnetic bearings:Current-mode implementation[J].IEEE/ASME Transactions on Mechatronics,2005,10(6):632-639.
[15] CHEN S,LIN F.Robust nonsingular terminal sliding-mode control for nonlinear magnetic bearing system[J].IEEE Transactions on Control Systems Technology,2011,19(3):636-643.
[16] GROCHMAL T,LYNCH A.Precision tracking of a rotating shaft with magnetic bearings by nonlinear decoupled disturbance observers[J].IEEE Transactions on Control Systems Technology,2007,15(6):1112-1121.
[17] 刘彬,房建成,刘刚.一种磁悬浮陀螺飞轮方案设计与关键技术分析[J].航空学报,2011,32(8):1478-1487.LIU B,FANG J C,LIU G.Design of a magnetically suspended gyrowheel and analysis of key technologies[J].Acta Aeronautica et Astronautica Sinica,2011,32(8):1478-1487(in Chinese). |