DocumentCode
605409
Title
Performance metrics for evaluating spacecraft power control and management (PCM)
Author
Madhusudhana, C.S. ; Kishore, J.K.
Author_Institution
ISRO Satellite Centre, Bangalore, India
fYear
2013
fDate
6-8 Feb. 2013
Firstpage
484
Lastpage
488
Abstract
The power subsystem is the most critical system in a spacecraft due to the dependency of nearly every other subsystem for power. The power system configuration depends on various factors such as amount of power required, type of orbit, duration of the mission, constraints on mass volume, and the impact of the system´s hardware on the spacecraft design. Power system encompasses power generation, energy storage and power processing. The organization of control and management circuits to carry out these functionalities is termed as Power Control and Management (PCM). Selection of an appropriate PCM is must for achieving the desired mission goal. This makes its choice a most important one for spacecraft Engineers. Different methods are adopted for finding out a suitable PCM. However availability of indices facilitate the evaluation of electrical performance of PCM systems. Hence a set performance metrics which would serve as benchmark has been detailed here. In the end, a typical case has been enumerated to demonstrate the usefulness of these metrics.
Keywords
power control; space power generation; control circuit; energy storage; management circuit; performance metrics; power generation; power management; power processing; spacecraft power control; Arrays; Batteries; Measurement; Phase change materials; Power systems; Space vehicles; Voltage control; Power control and management; array control; bus regulation; voltage ripple;
fLanguage
English
Publisher
ieee
Conference_Titel
Power, Energy and Control (ICPEC), 2013 International Conference on
Conference_Location
Sri Rangalatchum Dindigul
Print_ISBN
978-1-4673-6027-2
Type
conf
DOI
10.1109/ICPEC.2013.6527705
Filename
6527705
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