Spacecraft Power System Compatibility and Stability for the NASA EOS Satellite 929078
This paper addresses the problem of system stability of the NASA EOS satellite power system. A potential stability problem exists without a clear specification of the payload input impedance characteristic. Design guidelines are established for the control of the power system and the individual subcomponents to help insure stability with an unknown complex load. A testbed of the EOS power system is employed to verify the analysis.
Citation: Sable, D., Cho, B., and Lee, F., "Spacecraft Power System Compatibility and Stability for the NASA EOS Satellite," SAE Technical Paper 929078, 1992, https://doi.org/10.4271/929078. Download Citation
Author(s):
Dan M. Sable, Bo H. Cho, Fred C. Lee
Affiliated:
Virginia Polytechnic Institute and State Univ.
Pages: 6
Event:
27th Intersociety Energy Conversion Engineering Conference (1992)
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Satellites
Spacecraft
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