Robust Control of Aeronautical Electrical Generators for Energy Management Applications

被引:7
作者
Canciello, Giacomo [1 ]
Cavallo, Alberto [1 ]
Guida, Beniamino [1 ]
机构
[1] Univ Campania, Dept Ind & Informat Engn, I-81031 Aversa, Italy
关键词
SYNCHRONOUS GENERATOR; MODEL; DIFFERENTIATION; SYSTEMS;
D O I
10.1155/2017/1745154
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A new strategy for the control of aeronautical electrical generators via sliding manifold selection is proposed, with an associated innovative intelligent energy management strategy used for efficient power transfer between two sources providing energy to aeronautical loads, having different functionalities and priorities. Electric generators used for aeronautical application involve several machines, including a main generator and an exciter. Standard regulators (PI or PID-like) are normally used for the rectification of the generator voltage to be used to supply a high-voltage DC bus. The regulation is obtained by acting on a DC/DC converter that imposes the field voltage of the exciter. In this paper, the field voltage is fed to the generator windings by using a second-order sliding mode controller, resulting into a stable, robust (against disturbances) action and a fast convergence to the desired reference. By using this strategy, an energymanagement strategy is proposed that dynamically changes the voltage set point, in order to intelligently transfer power between two voltage busses. Detailed simulation results are provided in order to show the effectiveness of the proposed energy management strategy in different scenarios.
引用
收藏
页数:12
相关论文
共 36 条
[1]  
[Anonymous], 1978, SLIDING MODES THEIR
[2]  
[Anonymous], MIL STD 704F AIRCR E
[3]  
[Anonymous], 2002, IEEE PRESS POWER ENG
[4]   Limit cycles in control systems employing smart actuators with hysteresis [J].
Cavallo, A ;
Natale, C ;
Pirozzi, S ;
Visone, C .
IEEE-ASME TRANSACTIONS ON MECHATRONICS, 2005, 10 (02) :172-180
[5]   Output feedback control based on a high-order sliding manifold approach [J].
Cavallo, A ;
Natale, C .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 2003, 48 (03) :469-472
[6]  
Cavallo A., 2017, INT J ROBUST NONLINE
[7]   Supervised control of buck-boost converters for aeronautical applications [J].
Cavallo, Alberto ;
Canciello, Giacomo ;
Guida, Beniamino .
AUTOMATICA, 2017, 83 :73-80
[8]   Boost Full Bridge Bidirectional DC/DC Converter for Supervised Aeronautical Applications [J].
Cavallo, Alberto ;
Guida, Beniamino ;
Rubino, Luigi .
INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2014, 2014
[9]  
Cavallo A, 2012, IEEE DECIS CONTR P, P7088, DOI 10.1109/CDC.2012.6427026
[10]  
Cossar C., 2004, Second IEE International Conference on Power Electronics, Machines and Drives (Conference Publication No.498), P458