Model and Simulation of Permanent Magnets Synchronous Machine (PMSM) of the Electric Power Supply System (EPS), in Accordance with the Concept of a More Electric Aircraft (MEA)

Based on the mathematical model of synchronous electric machine, basing on permanent magnets, presented in this paper, the key importance of alternator AC power sources in the form of generator (for conventional aircraft) and in the form of integrated unit starter/AC synchronous generator S/G AC (with respect to advanced aircraft concept in the field of more/all electric power MEA/AEA) was highlighted. In addition, through the analysis and selected simulations of the power supply system of a modern aircrafts, sources of onboard electrical energy (synchronous generator, integrated unit starter/AC generator) were located in board autonomic power system ASE (EPS, PES). Key components of this system are the electro-energetic power system EPS and the energo-electronic power system PES. Additionally, the analysis and exemplary simulations of key electricity sources based on mathematical models have contributed to highlighting the main practical applications in line with the trend of a more electric aircraft.

[1]  Ian Moir,et al.  Design and Development of Aircraft Systems, Second Edition , 2012 .

[2]  T. L. Skvarenina,et al.  Simulation of a More-Electric Aircraft power system using an automated state model approach , 1996, IECEC 96. Proceedings of the 31st Intersociety Energy Conversion Engineering Conference.

[3]  Mike Barnes,et al.  Direct drive permanent magnet generator fed AC-DC active rectification and control for more-electric aircraft engines , 2011 .

[4]  Eric Monmasson,et al.  Field programmable gate array-based sensorless control of a brushless synchronous starter generator for aircraft application , 2011 .

[5]  Lucjan Setlak Overview of aircraft technology solutions compatible with the concept of mea , 2015 .

[6]  L. Setlak,et al.  Comparative Analysis and Simulation of Selected Components of Modern on-board Autonomous Power Systems ( ASE ) of Modern Aircraft in line with the Concept of MEA / AEA , 2022 .

[7]  Qiang Gao,et al.  Sensorless Operation of a Permanent Magnet Generator for Aircraft , 2005, IEEE International Conference on Electric Machines and Drives, 2005..

[8]  M. Abdel-Salam,et al.  ELECTRICAL DISTRIBUTION POWER SYSTEMS OF MODERN CIVIL AIRCRAFTS , 2013 .

[9]  Xudong Shi,et al.  Modeling and Simulation of Power Distribution System in More Electric Aircraft , 2015, J. Electr. Comput. Eng..

[10]  Mehrdad Ehsani,et al.  Aircraft power systems: technology, state of the art, and future trends , 2000 .

[11]  B. Singh,et al.  Analysis and design of STATCOM-based voltage regulator for self-excited induction generators , 2004, IEEE Transactions on Energy Conversion.

[12]  Josep M. Guerrero,et al.  Review of aircraft electric power systems and architectures , 2014, 2014 IEEE International Energy Conference (ENERGYCON).

[13]  Ian Moir,et al.  Civil Avionics Systems, Second Edition , 2013 .

[14]  Scott D. Sudhoff,et al.  Analysis of Electric Machinery and Drive Systems , 1995 .

[15]  Lucjan Setlak,et al.  Mathematical modeling and simulation of selected components on-board autonomous power supply system (ASE), in accordance with the concept of a more electric aircraft (MEA) , 2017, 2017 18th International Scientific Conference on Electric Power Engineering (EPE).

[16]  Ruofa Cheng,et al.  Modeling and Optimization Control for Aircraft AC Generator BrushlessExcitation System Based on Improved Adaptive PSO , 2015 .