Capel A, Perol P. Comparative performance evaluation between the S4R and the S3R regulated bus topologies[C]. IEEE Power Electronics Specialists Conf, 2001: 1963-1969.
[2]
A Capel O’Sullivan, J C Marpinard. High power conditioning for space applications[C]. IEEE Proceedings, 1988, 76: 201-210.
[3]
Dehbonei H, Lee S R, Ko S H. Direct energy transfer for high efficiency photovoltaic energy systems part I: concepts and hypothesis[J]. IEEE Transactions Aerospace and Electronic Systems, Jan 2009, 45: 31-45.
[4]
Dehbonei H, Lee S R, Ko S H. Direct energy transfer for high efficiency photovoltaic energy systems part II: experimental evaluations[J]. IEEE Transactions Aerospace and Electronic Systems, Jan 2009, 45: 46-57.
[5]
Blanes J M, Garrigos A, Carrasco J A, et al. Maximum power point estimator for photovoltaic solar arrays[C]. IEEE Mediterranean, Electronic technical Conference, 2006: 889-892.
[6]
E Maset, J B ejea, A Fereeres. New high power high voltage battery free bus for electrical propulsion in satellites[C]. Power Electronics Specialists Conference, IEEE PESC, 2007: 1391-1397.
Garrigos A, Carrasco J A, Blanes J M, et al. Modeling the sequential switching shunt series regulator[J]. IEEE Power Electronics Letters, 2005, 3(1): 7-13.
[9]
Garrigos A, Rubiato J, Carrasco J A, et al. System model of the sequential switching shunt series regulator for spacecraft regulated high power busses[C]. IEEE Power Electronics Specialists Conference, 2004: 2645-2650.
[10]
Garrigos A, Blanes J M, Carrasco J A, et al. A power conditioning unit for high power GEO satellites based on the sequential switching shunt series regulator[C]. IEEE Electrotechnical Conference, 2006: 1186-1189.
[11]
Garrigos A, Carrasco J A, Blanes J M, et al. A new sequential switching shunt regulator-digital shunt regulator (S3R-DSR) for solar array regulators[C]. IEEE Industrial Electronics Conference, 2006: 1064-1069.
[12]
Garrigos A, Rubiato J, et al. Control loop design of the sequential switching shunt series regulator[C]. IEEE Electrotechnical Conference, 2006: 1194-1197.
[13]
Maset E, Sanchis-Kilders E, Ejea J B, et al. New high power/high voltage battery-free bus for electrical propulsion in satellites[C]. IEEE APEC Conference, 2007: 1299-1305.
[14]
Dimroth, F Schubert, U Bette. 25.5% efficient Ga0.35In0.65P/Ga0.83 In0.17As tandem solar cells grown on GaAs substrates[J]. IEEE Electron Device Letters, 2000, 21(5): 209-211.
[15]
李国欣, 等. 航天器电源系统技术论述[M]. 北京: 宇航出版社, 2008.
[16]
Bruno ghislain liegeois. Switch shunt regulator and power supply arrangement using same for spacecraft applications: United States Patent, US6979986B2[P], 2005.
[17]
Garrigos A, Blanes J M, Carrasco J A, et al. Influence of the parasitic solar array capacitance in the sequential switching shunt series regulator[C]. IEEE Electrotechnical Conference, 2006: 1198-1201.
