New Electrical Power Supply System for All-Electric Propulsion Spacecraft

Ming Fu; Donglai Zhang; Tiecai Li

doi:10.1109/TAES.2017.2683638

New Electrical Power Supply System for All-Electric Propulsion Spacecraft

Ming Fu
, Donglai Zhang^*
, Tiecai Li

^*Corresponding author for this work

Harbin Institute of Technology Shenzhen
Shenzhen Academy of Aerospace Technology
School of Electrical Engineering and Automation, Harbin Institute of Technology

Research output: Contribution to journal › Article › peer-review

39 Scopus citations

Abstract

This paper proposes a novel electrical power supply system architecture (power conditioning and processing unit, PCPU) for high-power all-electric propulsion spacecraft platform with high-voltage power bus (HV_BUS) powering thrusters and regulated power bus (V_BUS) powering onboard payloads, respectively. The design principle of function modules in PCPU has been analyzed. Besides, the test on electrical characteristic of V_BUS and HV_BUS in prototyped system proves the stable and reliable work of buses in PCPU.

Original language	English
Article number	7880667
Pages (from-to)	2157-2166
Number of pages	10
Journal	IEEE Transactions on Aerospace and Electronic Systems
Volume	53
Issue number	5
DOIs	https://doi.org/10.1109/TAES.2017.2683638
State	Published - Oct 2017
Externally published	Yes

Keywords

All-electric propulsion (AEP)
domain control
power conditioning and processing unit (PCPU)
spacecraft power system

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10.1109/TAES.2017.2683638

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title = "New Electrical Power Supply System for All-Electric Propulsion Spacecraft",

abstract = "This paper proposes a novel electrical power supply system architecture (power conditioning and processing unit, PCPU) for high-power all-electric propulsion spacecraft platform with high-voltage power bus (HVBUS) powering thrusters and regulated power bus (VBUS) powering onboard payloads, respectively. The design principle of function modules in PCPU has been analyzed. Besides, the test on electrical characteristic of VBUS and HVBUS in prototyped system proves the stable and reliable work of buses in PCPU.",

keywords = "All-electric propulsion (AEP), domain control, power conditioning and processing unit (PCPU), spacecraft power system",

author = "Ming Fu and Donglai Zhang and Tiecai Li",

note = "Publisher Copyright: {\textcopyright} 2017 IEEE.",

year = "2017",

month = oct,

doi = "10.1109/TAES.2017.2683638",

language = "英语",

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N2 - This paper proposes a novel electrical power supply system architecture (power conditioning and processing unit, PCPU) for high-power all-electric propulsion spacecraft platform with high-voltage power bus (HVBUS) powering thrusters and regulated power bus (VBUS) powering onboard payloads, respectively. The design principle of function modules in PCPU has been analyzed. Besides, the test on electrical characteristic of VBUS and HVBUS in prototyped system proves the stable and reliable work of buses in PCPU.

AB - This paper proposes a novel electrical power supply system architecture (power conditioning and processing unit, PCPU) for high-power all-electric propulsion spacecraft platform with high-voltage power bus (HVBUS) powering thrusters and regulated power bus (VBUS) powering onboard payloads, respectively. The design principle of function modules in PCPU has been analyzed. Besides, the test on electrical characteristic of VBUS and HVBUS in prototyped system proves the stable and reliable work of buses in PCPU.

KW - All-electric propulsion (AEP)

KW - domain control

KW - power conditioning and processing unit (PCPU)

KW - spacecraft power system

UR - https://www.scopus.com/pages/publications/85032346618

U2 - 10.1109/TAES.2017.2683638

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JF - IEEE Transactions on Aerospace and Electronic Systems

IS - 5

M1 - 7880667

ER -

New Electrical Power Supply System for All-Electric Propulsion Spacecraft

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Keywords

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