面向机载脉冲负载的三相双输出整流器及其控制策略

doi:10.7527/S1000-6893.2025.31660

Abstract

Abstract:

A three-phase dual-output rectifier and its control strategy are proposed for powering airborne low-frequency pulsed load. To address the impact of high peak pulsed power load such as high-power airborne radar on the limited-capacity power supply system of aircraft， a rectifier is designed to simultaneously provide two independently controlled DC outputs. The two DC outputs are used to power the DC bus for the conventional loads and low-frequency pulsed load， respectively， solving the problem of low-frequency pulsed load interfering with the stable operation of conventional loads under the traditional single DC bus power supply architecture. By allowing the DC bus voltage for the low-frequency pulsed load to fluctuate over a wide range， the volume， capacity， and weight of the bus decoupling capacitors are significantly reduced. The paper presents the circuit implementation of the dual-output rectifier， provides a detailed analysis of its operating principles， and proposes a PWM modulation strategy and control method tailored to meet the power distribution and regulation requirements of the two outputs. Finally， experimental results are provided to validate the feasibility and effectiveness of the proposed method.

Key words: airborne power systems, pulsed power supply system, AC-DC converter, dual DC bus, pulsed power decoupling

CLC Number:

V242.2

Yubin DUAN, Xin JIN, Huimin YIN, Yan XING, Hongfei WU. Three-phase dual-output rectifier and its control strategy for airborne pulsed loads[J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(16): 331660.

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References 20

[1]	贲德. 机载有源相控阵火控雷达技术发展［J］. 现代雷达， 2024， 46（2）： 1-15.
	BEN D. Development of airborne AESA fire control radar［J］. Modern Radar， 2024， 46（2）： 1-15 （in Chinese）.
[2]	RODRIGUEZ M， ROBERG M， ZAI A， et al. Resonant pulse-shaping power supply for radar transmitters［J］. IEEE Transactions on Power Electronics， 2014， 29（2）： 707-718.
[3]	孟迪，张群，罗迎，等. 基于脉冲交错的数字阵列雷达任务优化调度算法［J］. 航空学报， 2017， 38（8）： 320930.
	MENG D， ZHANG Q， LUO Y， et al. An effective scheduling algorithm for digital array radar based on pulse interleaving［J］. Acta Aeronautica et Astronautica Sinica， 2017， 38（8）： 320930 （in Chinese）.
[4]	关中杰，鲁效平，李钢强，等. 基于风速模型的风电机组动态转矩前馈控制技术［J］. 电工技术学报， 2018， 33（22）： 5338-5345.
	GUAN Z J， LU X P， LI G Q， et al. Dynamic torque feed forward control technology of wind turbine based on wind speed model［J］. Transactions of China Electrotechnical Society， 2018， 33（22）： 5338-5345 （in Chinese）.
[5]	GAO F， YEOH S， BOZHKO S， et al. Coordinated control of a DC electrical power system in the more electric aircraft integrated with energy storage［C］∥2015 IEEE Energy Conversion Congress and Exposition （ECCE）. Piscataway： IEEE Press， 2015： 5431-5438.
[6]	MOHAMED A， SALEHI V， MOHAMMED O. Real-time energy management algorithm for mitigation of pulse loads in hybrid microgrids［J］. IEEE Transactions on Smart Grid， 2012， 3（4）： 1911-1922.
[7]	严鋆，王金全，陈颖，等. 基于开关函数的脉冲功率负载大信号模型研究［J］. 电工技术学报， 2020， 35（16）： 3509-3517.
	YAN J， WANG J Q， CHEN Y， et al. Study on large-signal model for pulsed power load based on switching functions［J］. Transactions of China Electrotechnical Society， 2020， 35（16）： 3509-3517 （in Chinese）.
[8]	MENG F G， XU X N， GAO L. A simple harmonic reduction method in multipulse rectifier using passive devices［J］. IEEE Transactions on Industrial Informatics， 2017， 13（5）： 2680-2692.
[9]	VITORINO M A， ALVES L F S， WANG R X， et al. Low-frequency power decoupling in single-phase applications： A comprehensive overview‍［J］. IEEE Transactions on Power Electronics， 2017， 32（4）： 2892-2912.
[10]	王立乔，崔舒敏，陈梅. 功率解耦型无电解电容PFC电路并联补偿控制［J］. 电工技术学报， 2019， 34（3）： 516-528.
	WANG L Q， CUI S M， CHEN M. Parallel compensation control of power factor corrector without electrolytic capacitor by power decoupling［J］. Transactions of China Electrotechnical Society， 2019， 34（3）： 516-528 （in Chinese）.
[11]	QIN S B， LEI Y T， BARTH C， et al. A high power density series-stacked energy buffer for power pulsation decoupling in single-phase converters［J］. IEEE Transactions on Power Electronics， 2017， 32（6）： 4905-4924.
[12]	杨洋，阮新波，叶志红. 无电解电容AC/DC LED驱动电源中减小输出电流脉动的前馈控制策略［J］. 中国电机工程学报， 2013， 33（21）： 18-25， 189.
	YANG Y， RUAN X B， YE Z H. A feed-forward scheme to reduce output current ripple of an electrolytic capacitor-less AC/DC LED driver［J］. Proceedings of the CSEE， 2013， 33（21）： 18-25， 189 （in Chinese）.
[13]	HUANG X Z， RUAN X B， DU F J， et al. A pulsed power supply adopting active capacitor converter for low-voltage and low-frequency pulsed loads［J］. IEEE Transactions on Power Electronics， 2018， 33（11）： 9219-9230.
[14]	SUN Y， LIU Y L， SU M， et al. Review of active power decoupling topologies in single-phase systems［J］. IEEE Transactions on Power Electronics， 2016， 31（7）： 4778-4794.
[15]	杨帆，李林，朱建鑫，等. 面向高峰均比低频脉冲功率负载的脉冲电流补偿器及其控制方法［J］. 电工技术学报， 2022， 37（16）： 4193-4201.
	YANG F， LI L， ZHU J X， et al. A pulsed current compensator and control strategy for high peak-to-average-ratio low frequency pulsed load‍［J］. Transactions of China Electrotechnical Society， 2022， 37（16）： 4193-4201 （in Chinese）.
[16]	ZHU J X， WU H F， CHEN J Y， et al. A hybrid three-phase AC/DC power system for low-frequency pulsed load applications‍［J］. IEEE Transactions on Industrial Electronics， 2021， 68（3）： 1871-1882.
[17]	李刚，陈洁，吴珩，等. 舰载相控阵雷达电源系统技术研究［J］. 雷达与对抗， 2018， 38（3）： 16-19.
	LI G， CHEN J， WU H， et al. Technologies of power system of shipborne phased array radar‍［J］. Radar & ECM， 2018， 38（3）： 16-19 （in Chinese）.
[18]	GAO X， WU H F， GAO S， et al. A two-stage pulsed power supply for low-DC-voltage and low-frequency pulsed-current loads‍［J］. IEEE Transactions on Power Electronics， 2021， 36（2）： 2298-2309.
[19]	李林，吴红飞，朱建鑫，等. 集成低频脉冲功率解耦端口的机载电源系统［J］. 航空学报， 2021， 42（6）： 624584.
	LI L， WU H F， ZHU J X， et al. Airborne power supply system integrating low-frequency pulse power decoupling port［J］. Acta Aeronautica et Astronautica Sinica， 2021， 42（6）： 624584 （in Chinese）.
[20]	张佐乾，吴红飞，杨帆，等. 基于部分功率调控的有源-无源电容分裂叠加式高峰均比低频脉冲功率平抑方法［J］. 中国电机工程学报， 2023， 43（3）： 1154-1163.
	ZHANG Z Q， WU H F， YANG F， et al. Partial power regulation-based high peak-to-average-ratio low-frequency pulse power suppression method with split active-passive capacitors superposition［J］. Proceedings of the CSEE， 2023， 43（3）： 1154-1163 （in Chinese）.

S_o	调制波与载波关系	开关导通状态	桥臂对地电压
0	v_a>v_ca	S_Z_x₁、S_Z_x₂开通 S_H_x 、S_L_x 关断	v₁
0	v_a<v_ca	S_L_x 、S_Z_x₂开通 S_H_x 、S_Z_x₁关断	0
1	v_a>v_ca	S_H_x 开通 S_Z_x₂、S_Z_x₁、S_L_x 关断	v₂
1	v_a<v_ca	S_L_x 开通 S_Z_x₂、S_Z_x₁、S_H_x 关断	0

参数	数值
交流输出电压有效值V_s/V	110
交流输出频率f_b/Hz	50
脉冲负载峰值电流I_p/A	8
脉冲负载谷值电流I_v/A	2
脉冲负载峰值电压V_2p/V	360
常规负载端口电压V₁/V	280
常规负载阻值R/Ω	100
脉冲负载母线电容C₂/mF	1
常规负载母线电容C₁/mF	1

Three-phase dual-output rectifier and its control strategy for airborne pulsed loads

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