Implementation and performance analysis of a novel sliding mode controller for bidirectional DC to DC converter in aircraft application

被引:0
作者
Karvekar, Aditi Sushil [1 ]
Joshi, Prasad [2 ]
机构
[1] Walchand Coll Engn, Dept Elect Engn, Sangli, India
[2] Govt Coll Engn Karad, Dept Elect Engn, Karad, India
关键词
More electric aircraft; Bidirectional DC to DC converter; PI controller; Sliding mode controller; ACTIVE BRIDGE CONVERTER; POWER-SYSTEMS; DESIGN; FUTURE; ARCHITECTURE;
D O I
10.1108/WJE-12-2022-0478
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
PurposeThe purpose of this paper is to implement a closed loop regulated bidirectional DC to DC converter for an application in the electric power system of more electric aircraft. To provide a consistent power supply to all of the electronic loads in an aircraft at the desired voltage level, good efficiency and desired transient and steady-state response, a smart and affordable DC to DC converter architecture in closed loop mode is being designed and implemented. Design/methodology/approachThe aircraft electric power system (EPS) uses a bidirectional half-bridge DC to DC converter to facilitate the electric power flow from the primary power source - an AC generator installed on the aircraft engine's shaft - to the load as well as from the secondary power source - a lithium ion battery - to the load. Rechargeable lithium ion batteries are used because they allow the primary power source to continue recharging them whenever the aircraft engine is running smoothly and because, in the event that the aircraft engine becomes overloaded during takeoff or turbulence, the charged secondary power source can step in and supply the load. FindingsA novel nonsingular terminal sliding mode voltage controller based on exponential reaching law is used to keep the load voltage constant under any of the aforementioned circumstances, and its performance is contrasted with a tuned PI controller on the basis of their respective transient and steady-state responses. The former gives a faster and better transient and steady-state response as compared to the latter. Originality/valueThis research gives a novel control scheme for incorporating an auxiliary power source, i.e. rechargeable battery, in more electric aircraft EPS. The battery is so implemented that it can get regeneratively charged when primary power supply is capable of handling an additional load, i.e. the battery. The charging and discharging of the battery is carried out in closed loop mode to ensure constant battery terminal voltage, constant battery current and constant load voltage as per the requirement. A novel sliding mode controller is used to improve transient and steady-state response of the system.
引用
收藏
页码:510 / 521
页数:12
相关论文
共 65 条
[1]  
Al-obaidi Nuha A., 2022, 2022 5th International Conference on Engineering Technology and its Applications (IICETA), P248, DOI 10.1109/IICETA54559.2022.9888704
[2]  
Alexander R, 2018, IEEE TRANSP ELECT C, P194, DOI 10.1109/ITEC.2018.8450240
[3]  
[Anonymous], 2016, 2016 IEEE EN CONV C, DOI DOI 10.1109/ECCE.2016.7854849
[4]  
Ansell PJ, 2022, IEEE ELECTRIF MAG, V10, P6, DOI 10.1109/MELE.2022.3165721
[5]   Electric Power Systems in More and All Electric Aircraft: A Review [J].
Barzkar, Ashkan ;
Ghassemi, Mona .
IEEE ACCESS, 2020, 8 (08) :169314-169332
[6]  
Benzaquen Joseph, 2021, CES Transactions on Electrical Machines and Systems, V5, P177, DOI 10.30941/CESTEMS.2021.00022
[7]   Identification and Descriptions of Fuel Cell Architectures for Aircraft Applications [J].
Bradley, Marty .
2022 IEEE/AIAA TRANSPORTATION ELECTRIFICATION CONFERENCE AND ELECTRIC AIRCRAFT TECHNOLOGIES SYMPOSIUM (ITEC+EATS 2022), 2022, :1047-1050
[8]  
Brombach J., 2012, Electrical Systems for Aircraft, Railway and Ship Propulsion (ESARS), P1, DOI DOI 10.1109/ESARS.2012.6387380
[9]   A Quadruple Active Bridge Converter for the Storage Integration on the More Electric Aircraft [J].
Buticchi, Giampaolo ;
Costa, Levy Ferreira ;
Barater, Davide ;
Liserre, Marco ;
Dominguez Amarillo, Eugenio .
IEEE TRANSACTIONS ON POWER ELECTRONICS, 2018, 33 (09) :8174-8186
[10]   Future of Electrical Aircraft Energy Power Systems: An Architecture Review [J].
Cano, Tania C. ;
Castro, Ignacio ;
Rodriguez, Alberto ;
Lamar, Diego G. ;
Khalil, Yehia F. ;
Albiol-Tendillo, Laura ;
Kshirsagar, Parag .
IEEE TRANSACTIONS ON TRANSPORTATION ELECTRIFICATION, 2021, 7 (03) :1915-1929