Simulation of AC spacecraft power systems
Abstract
This paper presents a technique for modeling and simulating ac spacecraft power systems. Each component in the spacecraft power system is treated as a two-port network. A state model is written for each two-port network with the port voltages as the inputs. Each component state model is solved using the state transition matrix approach. The inputs to each component are assumed constant for the solution of its state model. As a result, each component state model is solved independently of all other components. The inputs to all components are then calculated using network analysis principles.
- Authors:
-
- Auburn Univ., AL (USA). Dept. of Electrical Engineering
- Publication Date:
- OSTI Identifier:
- 5256503
- Resource Type:
- Journal Article
- Journal Name:
- IEEE Translations on Industrial Electronics; (USA)
- Additional Journal Information:
- Journal Volume: 36:3; Journal ID: ISSN 0278-0046
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 32 ENERGY CONSERVATION, CONSUMPTION, AND UTILIZATION; 21 SPECIFIC NUCLEAR REACTORS AND ASSOCIATED PLANTS; 99 GENERAL AND MISCELLANEOUS//MATHEMATICS, COMPUTING, AND INFORMATION SCIENCE; 24 POWER TRANSMISSION AND DISTRIBUTION; SPACECRAFT POWER SUPPLIES; SIMULATION; AC SYSTEMS; MATHEMATICAL MODELS; NETWORK ANALYSIS; ELECTRONIC EQUIPMENT; ENERGY SYSTEMS; EQUIPMENT; POWER SUPPLIES; POWER SYSTEMS; 320201* - Energy Conservation, Consumption, & Utilization- Transportation- Air & Aerospace; 220800 - Nuclear Reactor Technology- Propulsion Reactors; 990200 - Mathematics & Computers; 240201 - Power System Networks, Transmission & Distribution- AC Systems- (1990-)
Citation Formats
Nelms, R M, Evans, B W, and Grigsby, L L. Simulation of AC spacecraft power systems. United States: N. p., 1989.
Web. doi:10.1109/41.31503.
Nelms, R M, Evans, B W, & Grigsby, L L. Simulation of AC spacecraft power systems. United States. https://doi.org/10.1109/41.31503
Nelms, R M, Evans, B W, and Grigsby, L L. 1989.
"Simulation of AC spacecraft power systems". United States. https://doi.org/10.1109/41.31503.
@article{osti_5256503,
title = {Simulation of AC spacecraft power systems},
author = {Nelms, R M and Evans, B W and Grigsby, L L},
abstractNote = {This paper presents a technique for modeling and simulating ac spacecraft power systems. Each component in the spacecraft power system is treated as a two-port network. A state model is written for each two-port network with the port voltages as the inputs. Each component state model is solved using the state transition matrix approach. The inputs to each component are assumed constant for the solution of its state model. As a result, each component state model is solved independently of all other components. The inputs to all components are then calculated using network analysis principles.},
doi = {10.1109/41.31503},
url = {https://www.osti.gov/biblio/5256503},
journal = {IEEE Translations on Industrial Electronics; (USA)},
issn = {0278-0046},
number = ,
volume = 36:3,
place = {United States},
year = {Tue Aug 01 00:00:00 EDT 1989},
month = {Tue Aug 01 00:00:00 EDT 1989}
}
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