Adaptive state of energy evaluation for supercapacitor in emergency power system of more-electric aircraft

被引:16
|
作者
Wang, Bin [1 ]
Wang, Chaohui [1 ]
Wang, Zhiyu [1 ]
Ni, Siliang [2 ]
Yang, Yixin [1 ]
Tian, Pengyu [1 ]
机构
[1] Xi An Jiao Tong Univ, State Key Lab Mfg Syst Engn, Xian 710049, Shaanxi, Peoples R China
[2] Univ Canterbury, Coll Engn, Dept Mech Engn, Private Bag 4800, Christchurch 8140, New Zealand
基金
中国国家自然科学基金;
关键词
Supercapacitor; State of energy evaluation; Adaptive parameter estimation; Sliding mode observer; Emergency power system; More -electric aircraft; DOUBLE-LAYER CAPACITORS; MANAGEMENT STRATEGIES; CHARGE ESTIMATION; FUTURE; ARCHITECTURE; PARAMETERS; BATTERIES;
D O I
10.1016/j.energy.2022.125632
中图分类号
O414.1 [热力学];
学科分类号
摘要
This paper presents an adaptive state of energy (SOE) evaluation method for a supercapacitor in the emergency power system of a more-electric aircraft. The adaptive SOE evaluation is realized based on a dynamic first-order RC equivalent circuit and its self-adaptive updated parameters. First, a dynamic first-order RC equivalent circuit with three parameters (i.e., the charge/discharge resistance R0, the dynamic self-discharge resistance R1, and the dynamic capacity C1) and a state-space model are introduced for modeling the supercapacitor. Then, an adaptive sliding mode observer is designed for tracking the dynamic change of the three state-space model parameters (i. e., R0, (R0+R1)/R1C1, and 1/R1C1). With this design, the three parameters of the dynamic first-order RC equivalent circuit can be updated adaptively along with the derivation of the three state-space model parameters. Moreover, the adaptive sliding mode observer is redesigned with a sign function, which can enhance the convergence rate of the three self-adaptive updated parameters. Finally, the accurate SOE evaluation would be achieved based on the three self-adaptive updated parameters. Various simulations and experiments are con-ducted to validate the adaptive SOE evaluation method. It is shown that the adaptive SOE evaluation method can achieve 0.5% of the maximum relative error of the estimated SOE. Compared with the commonly used method, the adaptive SOE evaluation method has over 1% improvement for the SOE estimation accuracy.
引用
收藏
页数:10
相关论文
共 50 条
  • [41] Current Sharing in the High Voltage DC Parallel Electric Power System for the More Electric Aircraft
    Xu, Yanwu
    Zhang, Zhuoran
    Li, Jincai
    Yan, Yangguang
    2016 INTERNATIONAL CONFERENCE ON ELECTRICAL SYSTEMS FOR AIRCRAFT, RAILWAY, SHIP PROPULSION AND ROAD VEHICLES & INTERNATIONAL TRANSPORTATION ELECTRIFICATION CONFERENCE (ESARS-ITEC), 2016,
  • [42] An Enhanced Second Carrier Harmonic Cancellation Technique for Dual-Channel Enhanced Power Generation Centre Applications in More-Electric Aircraft
    Wang, Cheng
    Yang, Tao
    Kulsangcharoen, Ponggorn
    Bozhko, Serhiy
    IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2021, 68 (07) : 5683 - 5692
  • [43] Large-Signal Stability Study of Power System in More Electric Aircraft
    Chen, Jiawei
    Hou, Shuaicheng
    Wang, Chengjun
    2018 IEEE INTERNATIONAL POWER ELECTRONICS AND APPLICATION CONFERENCE AND EXPOSITION (PEAC), 2018, : 455 - 460
  • [44] A multi-agent approach to the more electric aircraft power system reconfiguration
    Bian, Xiangnan
    Ma, Qishuang
    Zhou, Yuying
    2007 IEEE INTERNATIONAL CONFERENCE ON MECHATRONICS AND AUTOMATION, VOLS I-V, CONFERENCE PROCEEDINGS, 2007, : 978 - +
  • [45] Impedance Modelling and Simulation of Variable Frequency AC Three-Stage Generator for More-Electric Aircraft
    Xu, Zixiao
    Zhao, Hongwei
    Qi, Yang
    Vasquez, Juan C.
    Guerrero, Josep M.
    Li, Weilin
    2023 25TH EUROPEAN CONFERENCE ON POWER ELECTRONICS AND APPLICATIONS, EPE'23 ECCE EUROPE, 2023,
  • [46] Optical Detection and Characteristics of PCB Partial Discharge in More-Electric Aircraft Under Square Wave Voltage
    Zang, Yiming
    Niasar, Mohamad Ghaffarian
    Xu, Yongpeng
    Li, Ze
    Qian, Qinglin
    Jiang, Xiuchen
    Vaessen, Peter
    IEEE JOURNAL OF EMERGING AND SELECTED TOPICS IN POWER ELECTRONICS, 2024, 12 (06) : 5558 - 5567
  • [47] Design of Partial-discharge-free Busbar for More-electric Aircraft Application with Low Pressure Condition
    Yuan, Zhao
    Wang, Yalin
    Wang, Zhongjing
    Emon, Asif Imran
    Peng, Hongwu
    Hassan, Mustafeez
    Narayanasamy, Balaji
    Luo, Fang
    2021 THIRTY-SIXTH ANNUAL IEEE APPLIED POWER ELECTRONICS CONFERENCE AND EXPOSITION (APEC 2021), 2021, : 1178 - 1182
  • [48] Regenerated Energy Absorption Methods for More Electric Aircraft Starter/Generator System
    Xu, Yanwu
    Zhang, Zhuoran
    IEEE TRANSACTIONS ON POWER ELECTRONICS, 2023, 38 (06) : 7525 - 7534
  • [49] Design and Optimization of Control System for More Electric Aircraft Power Systems Using Adaptive Tabu Search Algorithm Based on State-Variables-Averaging Model
    Phosung, Ratapon
    Areerak, Kongpan
    Areerak, Kongpol
    IEEE ACCESS, 2024, 12 : 76579 - 76588
  • [50] Dynamic Simulation of Battery/Supercapacitor Hybrid Energy Storage System for the Electric Vehicles
    Yaici, Wahiba
    Kouchachvili, Lia
    Entchev, Evgueniy
    Longo, Michela
    2019 8TH INTERNATIONAL CONFERENCE ON RENEWABLE ENERGY RESEARCH AND APPLICATIONS (ICRERA 2019), 2019, : 460 - 465