航空高压直流供电系统双向瞬态干扰抑制方法

doi:10.7527/S1000-6893.2024.30930

Abstract

Abstract:

In this paper， a suppression methodology based on the high voltage energy storage system and bidirectional energy conversion is proposed to solve the stability problem caused by the transient power demand of the radar/direct energy weapon and the bidirectional power flow of four-quadrant electric actuator. Firstly， a bidirectional energy control topology based on high-voltage battery and bidirectional power conversion is proposed， which uses the instantaneous charging and discharging of high-voltage battery to cut peaks and fill valleys to achieve bidirectional transient power control. Secondly， a comprehensive power supply management strategy based on bus voltage-load current and battery SOC is proposed to realize rapid detection of system load disturbance and fast configuration of power supply mode. Thirdly， a voltage stabilizing control method based on differential tracker and load current feedforward is proposed to improve the voltage performance of the converter under various loads. The simulation and experimental results show that the proposed method can effectively suppress the voltage fluctuation caused by high-power bidirectional transient load disturbance， and improve the robustness and quality of aerospace HVDC power supply system.

Key words: high voltage DC (HVDC) power supply system, bidirectional transient interference, battery control, Buck-Boost DC-DC converter, energy management, voltage regulation

CLC Number:

V242.2⁺31

Boyi ZHANG, Hong GUO, Jinquan XU, Longxian XUE, Zhongbing MA, Junxiang CHEN. Bidirectional transient interference suppression methodology in aviation HVDC electric power system[J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(7): 330930.

Figures/Tables 24

Fig.1

Fig.2

Table 1

Fig.3

Table 2

Fig.4

Table 3

Fig.5

Fig.6

Table 4

Transfer condition of distribution state machine

转移条件	通用条件	转移条件（电压/V、电压微分/（V·s^-1）、荷电状态/%、负载电流/A）
T01	① DC-DC通道正常&& ② 发电机正常	$u b u s < 260 V \| \| u b u s < 265 V & & u ˙ b u s < - 1 500 V · s - 1$
T10		$u b u s > 267$ $V$
T02		$u b u s > 280 V \| \| u b u s > 275 V & & u ˙ b u s > 1 500 V · s - 1$
T20		$u b u s < 273 V$
T03		$S O C < 70 %$
T30		$S O C > 80 %$
T04		$S O C > 90 % & & i l o a d > 10 A$
T40		$S O C < 80 % \| \| i l o a d < 8 A \| \| u b u s > 275 V \| \| u b u s < 265 V$
T15		$S O C < 70 %$
T51		$S O C > 80 %$
T35		$u b u s < 260 V \| \| u b u s < 265 V & & u ˙ b u s < - 1 500 V · s - 1$
T53		$u b u s > 267 V$
T26		$S O C < 70 %$
T62		$S O C > 80 %$
T36		$u b u s > 280 V \| \| u b u s > 275 V & & u ˙ b u s > 1 500 V · s - 1$
T63		$u b u s < 273 V$
T07	发电机故障	应急供电指令
T08	DC-DC通道故障	$u b u s > 280 V$ 开通IGBT $u b u s < 275 V$ 关断IGBT

Table 4

Fig.7

Fig.8

Fig.9

Fig.10

Fig.11

Fig.12

Fig.13

Fig.14

Fig.15

Fig.16

Fig.17

Fig.18

Fig.19

Fig.20

References 25

1	BARZKAR A， GHASSEMI M. Electric power systems in more and all electric aircraft： A review［C］∥IEEE Access. Piscataway： IEEE Press， 2020： 169314-169332.
2	CHEN J W， WANG C J， CHEN J. Investigation on the selection of electric power system architecture for future more electric aircraft［J］. IEEE Transactions on Transportation Electrification， 2018， 4（2）： 563-576.
3	张卓然，许彦武，于立，等. 多电飞机高压直流并联供电系统发展现状与关键技术［J］. 航空学报， 2021， 42（6）： 624069.
	ZHANG Z R， XU Y B， YU L， et al. Parallel HVDC electric power system for more-electric-aircraft： State of the art and key technologies［J］. Acta Aeronautica et Astronautica Sinica， 2021， 42（6）： 624069 （in Chinese）.
4	靳标，邝晓飞，彭宇，等. 基于合作博弈的组网雷达分布式功率分配方法［J］. 航空学报， 2022， 43（1）： 324776.
	JIN B， KUANG X F， PENG Y， et al. Distributed power allocation method for netted radar based on cooperative game theory［J］. Acta Aeronautica et Astronautica Sinica， 2022， 43（1）： 324776 （in Chinese）.
5	WHEELER P， TRENTIN A， BOZHKO S， et al. Regeneration of energy onto an aircraft electrical power system from an electro-mechanical actuator［C］∥2012 Electrical Systems for Aircraft， Railway and Ship Propulsion. Piscataway： IEEE Press， 2012： 1-6.
6	XU J Q， JIN W B， GUO H， et al. Modeling and analysis of oil frictional loss in wet-type permanent magnet synchronous motor for aerospace electro-hydrostatic actuator［J］. Chinese Journal of Aeronautics， 2023， 36（11）： 328-341.
7	HILL C I， BOZHKO S， YANG T， et al. More electric aircraft electro-mechanical actuator regenerated power management［C］∥2015 IEEE 24th International Symposium on Industrial Electronics （ISIE）. Piscataway： IEEE Press， 2015： 337-342.
8	WHEELER P W， CLARE J C， TRENTIN A， et al. An overview of the more electrical aircraft［J］. Proceedings of the Institution of Mechanical Engineers， Part G： Journal of Aerospace Engineering， 2013， 227（4）： 578-585.
9	ZHANG H， MOLLET F， SAUDEMONT C， et al. Experimental validation of energy storage system management strategies for a local DC distribution system of more electric aircraft［J］. IEEE Transactions on Industrial Electronics， 2010， 57（12）： 3905-3916.
10	TARIQ M， MASWOOD A I， GAJANAYAKE C J， et al. Modeling and integration of a lithiumion battery energy storage system with the more electric aircraft 270 V DC power distribution architecture［J］. IEEE Access， 2018， 6： 41785-41802.
11	ZHANG H， FAKHAM H， SAUDEMONT C， et al. Power management strategies in a local DC power distribution system of more electric aircraft with the help of hybrid storage and dissipation systems［C］∥2009 8th International Symposium on Advanced Electromechanical Motion Systems & Electric Drives Joint Symposium. Piscataway： IEEE Press， 2009： 1-7.
12	RECALDE A A， LUKIC M， HEBALA A， et al. Energy storage system selection for optimal fuel consumption of aircraft hybrid electric taxiing systems［J］. IEEE Transactions on Transportation Electrification， 2021， 7（3）： 1870-1887.
13	KLUMPNER C， RASHED M. Design and evaluation of a power converter for an energy storage system for aircrafts［C］∥2018 IEEE International Conference on Electrical Systems for Aircraft， Railway， Ship Propulsion and Road Vehicles & International Transportation Electrification Conference （ESARS-ITEC）. Piscataway： IEEE Press， 2018.
14	NAAYAGI R T， FORSYTH A J， SHUTTLEWORTH R. Performance analysis of extended phase-shift control of DAB DC-DC converter for aerospace energy storage system［C］∥2015 IEEE 11th International Conference on Power Electronics and Drive Systems. Piscataway： IEEE Press， 2015： 514-517.
15	WANG Y， XU F， MAO S W， et al. Adaptive online power management for more electric aircraft with hybrid energy storage systems［J］. IEEE Transactions on Transportation Electrification， 2020， 6（4）： 1780-1790.
16	WU D Y， TODD R， FORSYTH A. Advanced energy management control for energy storage system［C］∥7th IET International Conference on Power Electronics， Machines and Drives （PEMD 2014）. London： IET， 2014.
17	吴爱国，李际涛. DC-DC变换器控制方法研究现状［J］. 电力电子技术， 1999， 33（2）： 75-78.
	WU A G， LI J T. The present research on the control of DC-DC converter［J］. Power Electronics， 1999， 33（2）： 75-78 （in Chinese）.
18	夏宇航，王宇. 独立励磁直流发电系统优化控制方法比较［J］. 航空学报， 2023， 44（16）： 327975.
	XIA Y H， WANG Y. Comparative study on optimal control methods of independent excitation DC power generation system［J］. Acta Aeronautica et Astronautica Sinica， 2023， 44（16）： 327975 （in Chinese）.
19	ZHOU X S， SU D K， MA Y J， et al. Research on auto disturbance rejection control strategy of battery energy storage staggered parallel buck converter［C］∥2021 IEEE International Conference on Mechatronics and Automation （ICMA）. Piscataway： IEEE Press， 2021： 414-419.
20	SONG J， LIU Z T， SU H Y. A second-order sliding mode control design for bidirectional DCDC converter［C］∥2017 36th Chinese Control Conference （CCC）. Piscataway： IEEE Press， 2017： 9181-9186.
21	LEE Y T， CHIU C S， SHEN C T. Adaptive fuzzy terminal sliding mode control of DC-DC buck converters via PSoC［C］∥2010 IEEE International Conference on Control Applications. Piscataway： IEEE Press， 2010： 1205-1209.
22	LUO F， MA D S. Integrated adaptive step-up/down switching DCDC converter with tri-band tri-mode digital control for dynamic voltage scaling［C］∥2008 IEEE International Symposium on Industrial Electronics. Piscataway： IEEE Press， 2008： 142-147.
23	刘飞龙. 双有源桥DC/DC变换器调制优化及拓扑拓展研究［D］. 秦皇岛：燕山大学， 2018.
	LIU F L. Research on modulation optimization and topology expansion of dual active bridge DC/DC converter［D］.Qinhuangdao： Yanshan University， 2018 （in Chinese）.
24	ZHANG B Y， XU J Q， GUO H. Decoupling current sharing control for paralleled DC-DC converter in aerospace application［C］∥2021 24th International Conference on Electrical Machines and Systems （ICEMS）. Piscataway： IEEE Press， 2021： 218-222.
25	LIN X， XU J， ZHENG J. Small signal impedance based stability analysis of HVDC aircraft power system［C］∥CSAA/IET International Conference on Aircraft Utility Systems （AUS 2022）. London： IET， 2022： 273-278.

参数	数值
脉冲功率/kW	25
脉冲负载电流上升时间/ms	1
脉冲负载最长持续时间/ms	500
脉冲负载最短持续时间/ms	10
回馈功率/kW	10
回馈电流上升时间/ms	2
回馈过程持续时间/ms	15
应急供电功率/kW	25
应急供电时间/min	15

参数	数值
输入电压/V	200~350
输出电压/V	250~280
额定功率/kW	25
电感/μH	45
滤波电容/μF	200

[1]	Shuhao DENG, Tao LEI, Xianqiu JIN, Junxiang CHEN, Daiwen HUANG, Xiaobin ZHANG. Stability and power control method of hybrid power system for fuel cell UAVs [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(17): 530032-530032.
[2]	Yin DIAO, Zhi ZHANG, Yue PENG, Yang LI, Borong ZHANG, Zhiguo ZHANG. Energy management and trajectory optimization technology for rocket landing [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(15): 229634-229634.
[3]	Cheng HE, Yuqi TONG, Xinglu XIA, Gang CHEN. Integrated optimization of energy management strategy and mission path for hybrid-electric VTOL UAVs in cargo transportation [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(14): 229606-229606.
[4]	ZHU Bingjie, YANG Xixiang, ZONG Jian'an, DENG Xiaolong. Review of distributed hybrid electric propulsion aircraft technology [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(7): 25556-025556.
[5]	LIU Li, CAO Xiao, ZHANG Xiaohui, HE Yuntao. Review of development of light and small scale solar/hydrogen powered unmanned aerial vehicles [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(3): 623474-623474.
[6]	ZHONG Weiguo, GUO Youguang, ZHANG Kai. Energy strategy on altitude profile for cycle flight of solar powered aircraft [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(3): 623429-623429.
[7]	ZHU Lihong, SUN Guorui, HU Wentao, LI Chuan, FU Zengying, YU Zhihang, LIU Zhengxin. Key technology and development trend of energy system in solar powered unmanned aerial vehicles [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(3): 623503-623503.
[8]	WU Jianfa, WANG Honglun, HUANG Yu. Research development of solar powered UAV mission planning technology in large-scale time and space spans [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(3): 623414-623414.
[9]	LEI Tao, MIN Zhihao, FU Hongjie, ZHANG Xingyu, LI Weilin, ZHANG Xiaobin. Dynamic balanced energy management strategies for fuel-cell hybrid power system of unmanned air vehicle [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(12): 324048-324048.
[10]	ZHANG Xiaohui, LIU Li, DAI Yueling. Coupling effect of energy management and flight state for fuel cell powered UAVs [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(7): 222793-222793.
[11]	ZHANG Xiaohui, LIU Li, Dai Yueling, SHEN Hui. Design and test of propulsion system for fuel cell powered UAVs [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(8): 221874-221874.
[12]	FAN Pengfei, LIU Jiaolong, FAN Yonghua, YAN Jie. In-flight TAEM guidance based on parameterized trajectory [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(12): 322382-322382.
[13]	ZANG Xiheng, HU Yongtai. Trajectory design for terminal area energy management of suborbital reusable launch vehicle [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(S1): 99-105.
[14]	LIU Li, DU Mengyao, ZHANG Xiaohui, ZHANG Chao, XU Guangtong, WANG Zhengping. Conceptual design and energy management strategy for UAV with hybrid solar and hydrogen energy [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(1): 144-162.
[15]	WANG Li;YANG Shan-shui;ZHANG Zhuo-ran;YAN Yang-guang. Application of Load Current Feedback Compensating in Digital Voltage Regulation for Doubly Salient Brushless DC Generator [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2006, 27(5): 934-938.

Bidirectional transient interference suppression methodology in aviation HVDC electric power system

RichHTML

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

Figures/Tables 24

References 25

Related Articles 15

Recommended Articles

Metrics

Comments