Nicolas N, Didier L, Peter A, et al. A new modular and flexible power system for LEO missions[C]. Proceedings of 9th European Space Power Conference, 2011: SP-690.
[2]
Morsaniga P, Gervasio G, Cuzzocrea G. Bepicolombo electrical power system[C]. Proceedings of 9th European Space Power Conference, 2011: SP-690.
[3]
Dan O. Lessons learnt in-flight-the STRV micro- satellite power system[C]. Proceedings of 4th European Space Power Conference, 1995: 257-261.
[4]
Sullivan D O. Space power electronics-design drivers[J]. Ecological Society of America, 1994, 1: 18.
[5]
Wolfgang D, Willi D. Generic 100V/high power bus conditioning[C]. Proceedings of 7th European Space Power Conference, 2005: SP-589.
[6]
Soubrier L, Trehet E. High power PCU for alphabus: PSR100V[C]. Proceedings of 9th European Space Power Conference, 2011: SP-690.
[7]
Soubrier L, B Patrick. High performance BDR for the PCU of alphabus[C]. Proceedings of 8th European Space Power Conference, 2008: SP-661.
[8]
Maset E, Sanchis Kilders E, Weinberg A H, et al. Ion drive propulsion MPP power conditioning system without battery[C]. Proceedings of 8th European Space Power Conference, 2008: SP-661.
[9]
Maset E, Ferrers A. 5kW Weinberg converter for battery discharging in high-power communications satellites[C]. Proceedings of IEEE Power Electronics Specialist Conference, 2005: 69-75.
[10]
Weinberg A H, P Rueda Boldo. A high power, high frequency, DC to DC converter for space applications [C]. Proceedings of IEEE Power Electronics Specialist Conference, 1992: 1140-1147.
