21 |
Power system control and stability evaluation using a separation surface techniqueNourmoussavi Nassab, Miraboutaleb. January 1980 (has links)
No description available.
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22 |
Power System Design, Analysis, and Power Electronics Implementation on Generic Nanosatellite Bus (GNB) SpacecraftBonin, Grant 16 February 2010 (has links)
The development of a multi-mission small spacecraft power system is described. This system has been designed for the University of Toronto Space Flight Laboratory Generic Nanosatellite Bus (GNB), an approximately 20cm cubical spacecraft with no deployed solar arrays. The GNB is inherently power-generation limited, and consequently, all available power must be utilized with maximum efficiency. This efficiency is achieved using an unconventional parallel-regulated architecture with Peak Power Tracking (PPT) functionality, and is shown to be the PPT design of highest efficiency for spacecraft of this class. In support of this design, a novel spacecraft power simulation suite has been developed, enabling parametric satellite power analysis with high fidelity. Finally, a unique variation on peak power tracking---referred to as peak current tracking---is described. This method is shown to reduce battery depth-of-discharge by as much as 20% over baseline architectures, and furthermore exhibits beneficial emergent behaviour for battery charge management.
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23 |
Power System Design, Analysis, and Power Electronics Implementation on Generic Nanosatellite Bus (GNB) SpacecraftBonin, Grant 16 February 2010 (has links)
The development of a multi-mission small spacecraft power system is described. This system has been designed for the University of Toronto Space Flight Laboratory Generic Nanosatellite Bus (GNB), an approximately 20cm cubical spacecraft with no deployed solar arrays. The GNB is inherently power-generation limited, and consequently, all available power must be utilized with maximum efficiency. This efficiency is achieved using an unconventional parallel-regulated architecture with Peak Power Tracking (PPT) functionality, and is shown to be the PPT design of highest efficiency for spacecraft of this class. In support of this design, a novel spacecraft power simulation suite has been developed, enabling parametric satellite power analysis with high fidelity. Finally, a unique variation on peak power tracking---referred to as peak current tracking---is described. This method is shown to reduce battery depth-of-discharge by as much as 20% over baseline architectures, and furthermore exhibits beneficial emergent behaviour for battery charge management.
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24 |
Bulk transmission system reliability analysis of protection and control groupsKumbale, Murali 05 1900 (has links)
No description available.
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25 |
Application of balanced realizations to power system equivalentsTroullinos, George 05 1900 (has links)
No description available.
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26 |
A general approach to network equivalents for on-line power system security assessmentContaxis, George Constantinos 05 1900 (has links)
No description available.
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27 |
A general approach to the calculation of reliability indices for an electric power transmission systemHayes, Thomas Pierce 12 1900 (has links)
No description available.
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28 |
Real-time modelling of multimachine power systemsDale, L. A. January 1986 (has links)
No description available.
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29 |
Evaluation of unit commitment techniques for the economic scheduling of thermal unitsBond, S. D. January 1985 (has links)
No description available.
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30 |
Short-term coordination and fast-recoordination of hydrothermal systems : a new approach using the continuation methodCalderon Giron, L. Rodolfo (Luis Rodolfo) January 1985 (has links)
No description available.
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