Design of a battery charger for the NASA EOS space platformA battery charger design for the NASA Earth Observing System (EOS) space platform has been developed and tested. The authors discuss the design of the battery charger power state and its current and voltage control loops. In addition to restoring energy to the batteries, this charger regulates the spacecraft bus voltage during the posteclipse transition period. The battery charger design and analysis were facilitated by use of the pulse-width-modulated (PWM) switch model and the new continuous-time model for current-mode control. Analyses of the battery charger small-signal behavior are compared to hardware measurements to verify modeling accuracy.
Document ID
19920067988
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sizemore, Tom (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Lee, Fred C. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Cho, Bo H. (Virginia Polytechnic Institute and State University Blacksburg, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: IECEC ''91: Intersociety Energy Conversion Engineering Conference