[1] Graver B, Zhang K, Rutherford D. emissions from commercial aviation, 2018. International Council on Clean Transportation.
[2] Kılkış Ş, Kılkış Ş. Benchmarking aircraft metabolism based on a sustainable airline index. Journal of cleaner production. 2017;167:1068-83. DOI 10.1016/j.jclepro.2017.03.183
[3] IATA. Climate change & CORSIA; 2018.
[4] Pourbafarani Z, Montazeri-Gh. Gear shift controller design in electric hybrid vehicle with AMT gearbox. Aerospace Mechanics. 2012;8(3). (In Persian).
[5] Zhang J, Roumeliotis I, Zolotas A. Nonlinear model predictive control-based optimal energy management for hybrid electric aircraft considering aerodynamics-propulsion coupling effects. IEEE Transactions on transportation electrification. 2021;8(2):2640-53. DOI 10.1109/TTE.2021.3137260
[6] Antcliff KR, Capristan FM. Conceptual design of the parallel electric-gas architecture with synergistic utilization scheme (PEGASUS) concept. In18th AIAA/ISSMO multidisciplinary analysis and optimization conference 2017 (p. 4001). DOI 10.2514/6.2017-4001
[7] Wroblewski GE, Ansell PJ. Hybrid-electric regional jet aircraft operation efficiency. In2019 AIAA/IEEE Electric Aircraft Technologies Symposium (EATS) 2019 (pp. 1-22). IEEE.. DOI 10.2514/6.2019-4397
[8] Lee B, Kwon S, Park P, Kim K. Active power management system for an unmanned aerial vehicle powered by solar cells, a fuel cell, and batteries. IEEE transactions on aerospace and electronic systems. 2014;50(4):3167-77. DOI 10.1109/TAES.2014.130468
[9] Zhang X, Liu L, Dai Y. Fuzzy state machine energy management strategy for hybrid electric UAVs with PV/fuel cell/battery power system. International Journal of Aerospace Engineering. 2018;2018(1):2852941. DOI 10.1155/2018/2852941
[10] Xie Y, Savvaris A, Tsourdos A. Fuzzy logic based equivalent consumption optimization of a hybrid electric propulsion system for unmanned aerial vehicles. Aerospace Science and Technology. 2019;85:13-23. DOI 10.1016/j.ast.2018.12.001
[11] Voskuijl M, Van Bogaert J, Rao AG. Analysis and design of hybrid electric regional turboprop aircraft. CEAS Aeronautical Journal. 2018;9(1):15-25. DOI 10.1007/s13272-017-0272-1
[12] Rendón MA, Assato M, Martins VA, Hallak PH, Altgott AS, Graca R, Landy Z, Oliveira NL, Delmonte RG. Design method and performance analysis of a hybrid-electric power-train applied in a 30-passenger aircraft. Journal of Cleaner Production. 2022;339:130560. DOI 10.1016/j.jclepro.2022.130560
[13] Cameretti MC, Del Pizzo A, Di Noia LP, Ferrara M, Pascarella C. Modeling and investigation of a turboprop hybrid electric propulsion system. Aerospace. 2018;5(4):123. DOI 10.3390/aerospace5040123
[14] Quillet D, Boulanger V, Rancourt D, Freer R, Bertrand P. Parallel hybrid-electric powertrain sizing on regional turboprop aircraft with consideration for certification performance requirements. InAIAA Aviation 2021 Forum 2021 (p. 2443). DOI 10.2514/6.2021-2443
[15] Federal Aviation Administration and Aerospace Industries Association, (1999), “Technical Report on Propulsion System and Auxiliary Power Unit (APU) Related Aircraft Safety Hazards,” October 25, 1999.
[16] Federal Aviation Administration and Aerospace Industries Association, (2005), “2nd Technical Report on Propulsion System and Auxiliary Power Unit (APU) Related Aircraft Safety Hazards,” January 31, 2005.
[17] Federal Aviation Administration and Aerospace Industries Association, (2017), “3rd Technical Report on Propulsion System and Auxiliary Power Unit (APU) Related Aircraft Safety Hazards,” March 30, 2017.
[18] Astridge DG. Helicopter transmissions—Design for safety and reliability. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 1989;203(2):123-38. DOI 10.1243/PIME_PROC_1989_203_063_01
[19] Davies DP, Jenkins SL, Belben FR. Survey of fatigue failures in helicopter components and some lessons learnt. Engineering Failure Analysis. 2013;32:134-51. DOI 10.1016/j.engfailanal.2013.03.005
[20] Karmakar S, Chattopadhyay S, Mitra M, Sengupta S. Induction motor and faults. InInduction motor fault diagnosis: approach through current signature analysis 2016 (pp. 7-28). Singapore: Springer Singapore. DOI 10.1007/978-981-10-0624-1
[21] Armstrong M, Ross C, Phillips D, Blackwelder M. Stability, transient response, control, and safety of a high-power electric grid for turboelectric propulsion of aircraft. 2013.
[22] Kastha D, Bose BK. Investigation of fault modes of voltage-fed inverter system for induction motor drive. IEEE transactions on industry applications. 2002;30(4):1028-38. DOI 10.1109/28.297920
[23] Zhang W, Xu D, Enjeti PN, Li H, Hawke JT, Krishnamoorthy HS. Survey on fault-tolerant techniques for power electronic converters. IEEE Transactions on Power Electronics. 2014;29(12):6319-31. DOI 10.1109/TPEL.2014.2304561
[24] Williard N, He W, Hendricks C, Pecht M. Lessons learned from the 787 dreamliner issue on lithium-ion battery reliability. Energies. 2013;6(9):4682-95. DOI 10.3390/en6094682
[25] U.S. Department of Transportation National Highway Traffic Safety Administration, “Lithium-ion Battery Safety Issues for Electric and Plug-in Hybrid Vehicles,” DOT HS 812 418.
[26] Montazeri-Gh, Khasheinejad M. Modeling and Simulation of Hybrid Propulsion System For Regional Aircraft. 7th National Gas Turbine Conference, Tehran. 2023. (In Persian).
[27] ATR. ATR 42-600 Regional Aircraft Data Summary. https://www.atr-aircraft.com/our-aircraft/atr-42-600/. [Accessed: 11-Nov-2020].
[28] Ballin MG. A High Fidelity Real-Time Simulation of a Small Turboshaft Engine. 1988.