航天用带耦合电感的电流连续型推挽类拓扑研究

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Abstract Considering the merits of high power density, high efficiency and low EMI, the DC-DC converter with continuous current is competitive in the application of spacecraft. The concept of continuous current push-pull based topology with coupling inductor is proposed in this paper. In order to obtain continuous current, five new push-pull cells are deduced from traditional push-pull cell. According to the novel structure of continuous current push-pull based topology with coupling inductor, the generation rule is proposed and the topologies based on five new push-pull cells are deduced separately. Depending on the condition that the current of bus side is low-ripple, these topologies are chosen as battery discharge regulator(BDR) or battery charge regulator(BCR). The characteristics are compared to provide optimal topology choice for BDR and BCR. Lastly, a prototype based on a generated topology with high voltage gain is designed and made to verify the correctness of theoretical analysis.

Key words： Power conditioning unit coupling inductor continuous current push-pull based topology combination rule

Received: 20 September 2012 Published: 05 November 2014

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TM134

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	Chen Qian
	Trillion Q. Zheng
	Li Yan

Cite this article:

Chen Qian,Trillion Q. Zheng,Li Yan. Continuous Current Push-Pull Based Topology with Coupling Inductor Used in Spacecraft[J]. Transactions of China Electrotechnical Society, 2014, 29(10): 1-11.

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http://dgjsxb.ces-transaction.com/EN/ OR http://dgjsxb.ces-transaction.com/EN/Y2014/V29/I10/1

[1] Nelson R F, Kepros M A, AC ripple effects on VRLA batteries in float applications[C]. Proceedings of the 14th BCAA, 1999: 281-289.
[2] Choi W, Enjeti P N, Howze J W. Development of an equivalent circuit model of a fuel cell to evaluate the effects of inverter ripple current[C]. Proceedings of the 19th Applied Power Electronics Conference, 2004: 355-361.
[3] Hansen M M. Power conditioning unit for bepicolombo transfer module[C]. Proceedings of the 8th European Space Power Conference, 2008.
[4] Jensen H, Laursen J. Power conditioning unit for Rosetta/Mars express[C]. Proceedings of the 6th European Space Power Conference, 2002: 249-256.
[5] 赵春阳,陈洪涛. 100V母线10kW级电源控制装置发展初探[J]. 电源技术, 2008, 32(9): 628-630. Zhao Chunyang, Chen Hongtao. Development of the 100 V-10 kW power conditioning unit[J]. Chinese Journal of Power Sources, 2008, 32(9): 628-630.
[6] Castiaux J P, Lecomte E, Labille J M, et al. Modular high power conditioning unit[C]. Proceedings of the 5th European Space Power Conference, 1998: 99-104.
[7] Garrigos A, Carrasco J A, Blanes J M, et al. A power conditioning unit for high power GEO satellites based on the sequential switching shunt series regulator[C]. Proceedings of the Miditerranean Electrotechnical Conference, 2006: 1186-1189.
[8] Patel M. Spacecraft power system[M]. United States: CRC Press Inc., 2005.
[9] Soubrier L, Besdel P, Daubresse T, et al. High performance BDR for the PCU of alphabus[C]. Procee- dings of the 8th European Space Power Conference, 2008.
[10] Roinila T, Hankaniemi M, Suntio T, et al. Dynamical profile of a switched-mode converter reality or imagina- tion[C]. Proceedings of the 29th International Telec- ommunications Energy Conference, 2007: 420- 427.
[11] Sammaljarvi T, Lakhdari F, Karppanen M, et al. Modelling and dynamic characterisation of peak current mode controlled superboost converter[J]. IET Power Electronics, 2008, 4(1): 527-536.
[12] Aroca J, Olsson D, Maicas J. An efficient BDR topology, able to handle a large battery voltage range[C]. Proceedings of the 5th European Space Power Conference, 1999.
[13] Weinberg A H, Rueda Boldo P. A high power, high frequency, DC to DC converter for space applications [C]. Proceedings of the IEEE Power Electronics Specialists Conference, 1992: 1140-1147.
[14] Maset E, Ejea J B, Ferreres A. High-efficiency weinberg converter for battery discharging in aerospace applications[C]. Proceedings of the IEEE Applied Power Electronics Conference, 2006, 1510- 1516.
[15] Maset E, Ferrers A. 5kW Weinberg converter for battery discharging in high-power communications satellites[C]. Proceedings of the IEEE Power Electronics Specialists Conference, 2005: 69-75.
[16] Weinberg A H. The battery discharge of the galileo satellite test bed-V2A power system using the weinberg topology[C]. Proceedings of the 7th European Space Power Conference, 2005.
[17] Denzinger W, Dietrich W. Generic 100V/high power bus conditioning[C]. Proceedings of the 7th European Space Power Conference, 2005.