This paper proposes a novel electrical power supply system architecture (power
conditioning and processing unit, PCPU) for high-power all-electric propulsion spacecraft …

Even for short space flights, such as manned flights to the Moon back in the 60s, it became
extremely obvious that electric batteries are completely unsuitable because of their huge …

Satellite dc-dc power converters are required to have electromagnetic interference (EMI)
compatibility as well as high reliability. The requirement of high reliability limits the …

The conventional Weinberg converter, owing to its high efficiency, continuous input and
output current, and the soft switching of its switches and diodes, is essentially utilized in …

Despite metrological limitations, photovoltaic (PV) cells can be used as orbital sensors in
order to evaluate sunlight incidence angles, sun position, and angular rates with acceptable …

The power supply subsystem of satellite is the core constant, throughout the whole flight
stage. The solar array-battery power system is the main selection for the regulated bus …

Актуальность темы. Разработка систем электропитания (СЭП) космических аппаратов
(КА) осуществляется по критерию экстремума энергомассовых характеристик. Это …

借鉴航天器一次电源系统顺序开关分流调节器(sequential switching shunt regulator, S3R)
架构, 针对新能源应用进行太阳阵分流器的研究, 该方法理论上可进行任意功率水平的扩展; …

Take the case of parallel modules in battery discharging regulator of power conditioning
unit, which is based on Weinberg topology, a conductance compensator used in average …

A method of synthesizing a digital controller for a solar energy conversion channel in a
power supply system of a spacecraft is presented. The method is based on the initial …