The Experts below are selected from a list of 43530 Experts worldwide ranked by ideXlab platform
J M Undrill - One of the best experts on this subject based on the ideXlab platform.
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An interim dynamic induction motor model for stability studies in the WSCC
2003 IEEE Power Engineering Society General Meeting (IEEE Cat. No.03CH37491), 2003Co-Authors: L Pereira, D Kosterev, P Mackin, D Davies, J M Undrill, Wenchun ZhuAbstract:Summary form only given. An "interim" composite load containing a static part and a dynamic part has been implemented in the WSCC. The static part of the load model is about 80% of the total load and comprises of existing static load data from the WSCC members. The dynamic part is a default induction motor model for approximately 20% of the total load. This composite model is used for all loads in the full-scale WSCC grid models that are the basis for System Interconnection studies. The model is designed primarily to capture the effects of dynamic induction motor loads for highly stressed north to south flow conditions during summer peaks in the WSCC.
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an interim dynamic induction motor model for stability studies in the wscc
IEEE Transactions on Power Systems, 2002Co-Authors: L Pereira, D Kosterev, P Mackin, D Davies, J M UndrillAbstract:An "interim" composite load model containing a static part and a dynamic part has been implemented in the Western Systems Coordinating Council (WSCC). The static part of the load model is about 80% of the total load and comprises of existing static load data from the WSCC members. The dynamic part is a default induction motor model for approximately 20% of the total load. This composite model is used for all loads in the full-scale WSCC grid models that are the basis for System Interconnection studies. The model is designed primarily to capture the effects of dynamic induction motor loads for highly stressed north to south flow conditions during summer peaks in the WSCC.
Scott C. Burleigh - One of the best experts on this subject based on the ideXlab platform.
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survey of inter satellite communication for small satellite Systems physical layer to network layer view
arXiv: Networking and Internet Architecture, 2016Co-Authors: Radhika Radhakrishnan, William W. Edmonson, Fatemeh Afghah, Frank Pinto, Ramon Martinez Rodriguezosorio, Scott C. BurleighAbstract:Small satellite Systems enable whole new class of missions for navigation, communications, remote sensing and scientific research for both civilian and military purposes. As individual spacecraft are limited by the size, mass and power constraints, mass-produced small satellites in large constellations or clusters could be useful in many science missions such as gravity mapping, tracking of forest fires, finding water resources, etc. Constellation of satellites provide improved spatial and temporal resolution of the target. Small satellite constellations contribute innovative applications by replacing a single asset with several very capable spacecraft which opens the door to new applications. With increasing levels of autonomy, there will be a need for remote communication networks to enable communication between spacecraft. These space based networks will need to configure and maintain dynamic routes, manage intermediate nodes, and reconfigure themselves to achieve mission objectives. Hence, inter-satellite communication is a key aspect when satellites fly in formation. In this paper, we present the various researches being conducted in the small satellite community for implementing inter-satellite communications based on the Open System Interconnection (OSI) model. This paper also reviews the various design parameters applicable to the first three layers of the OSI model, i.e., physical, data link and network layer. Based on the survey, we also present a comprehensive list of design parameters useful for achieving inter-satellite communications for multiple small satellite missions. Specific topics include proposed solutions for some of the challenges faced by small satellite Systems, enabling operations using a network of small satellites, and some examples of small satellite missions involving formation flying aspects.
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Survey of Inter-Satellite Communication for Small Satellite Systems: Physical Layer to Network Layer View
IEEE Communications Surveys & Tutorials, 2016Co-Authors: Radhika Radhakrishnan, William W. Edmonson, Fatemeh Afghah, Ramon Martinez Rodriguez-osorio, Frank Pinto, Scott C. BurleighAbstract:Small satellite Systems enable a whole new class of missions for navigation, communications, remote sensing, and scientific research for both civilian and military purposes. As individual spacecraft are limited by the size, mass, and power constraints, mass-produced small satellites in large constellations or clusters could be useful in many science missions such as gravity mapping, tracking of forest fires, finding water resources, etc. The proliferation of small satellites will enable a better understanding of the near-Earth environment and provide an efficient and economical means to access the space through the use of multi-satellite solution. Constellation of satellites provide improved spatial and temporal resolution of the target. Small satellite constellations contribute innovative applications by replacing a single asset with several very capable spacecraft, which opens the door to new applications. Future space missions are envisioned to become more complex and operate farther from Earth, and will need to support autonomous operations with minimal human intervention. With increasing levels of autonomy, there will be a need for remote communication networks to enable communication between spacecraft. These space-based networks will need to configure and maintain dynamic routes, manage intermediate nodes, and reconfigure themselves to achieve mission objectives. Hence, inter-satellite communication is a key aspect when satellites fly in formation. In this survey, we present the various research being conducted in the small satellite community for implementing inter-satellite communications based on the open System Interconnection (OSI) model. This survey also reviews the various design parameters applicable to the first three layers of the OSI model, i.e., physical, data link, and network layer. Based on the survey, we also present a comprehensive list of design parameters useful for achieving inter-satellite communications for multiple small satellite missions. Specific topics include proposed solutions for some of the challenges faced by small satellite Systems, enabling operations using a network of small satellites, and some examples of small satellite missions involving formation flying aspects.
L Pereira - One of the best experts on this subject based on the ideXlab platform.
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An interim dynamic induction motor model for stability studies in the WSCC
2003 IEEE Power Engineering Society General Meeting (IEEE Cat. No.03CH37491), 2003Co-Authors: L Pereira, D Kosterev, P Mackin, D Davies, J M Undrill, Wenchun ZhuAbstract:Summary form only given. An "interim" composite load containing a static part and a dynamic part has been implemented in the WSCC. The static part of the load model is about 80% of the total load and comprises of existing static load data from the WSCC members. The dynamic part is a default induction motor model for approximately 20% of the total load. This composite model is used for all loads in the full-scale WSCC grid models that are the basis for System Interconnection studies. The model is designed primarily to capture the effects of dynamic induction motor loads for highly stressed north to south flow conditions during summer peaks in the WSCC.
-
an interim dynamic induction motor model for stability studies in the wscc
IEEE Transactions on Power Systems, 2002Co-Authors: L Pereira, D Kosterev, P Mackin, D Davies, J M UndrillAbstract:An "interim" composite load model containing a static part and a dynamic part has been implemented in the Western Systems Coordinating Council (WSCC). The static part of the load model is about 80% of the total load and comprises of existing static load data from the WSCC members. The dynamic part is a default induction motor model for approximately 20% of the total load. This composite model is used for all loads in the full-scale WSCC grid models that are the basis for System Interconnection studies. The model is designed primarily to capture the effects of dynamic induction motor loads for highly stressed north to south flow conditions during summer peaks in the WSCC.
Radhika Radhakrishnan - One of the best experts on this subject based on the ideXlab platform.
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survey of inter satellite communication for small satellite Systems physical layer to network layer view
arXiv: Networking and Internet Architecture, 2016Co-Authors: Radhika Radhakrishnan, William W. Edmonson, Fatemeh Afghah, Frank Pinto, Ramon Martinez Rodriguezosorio, Scott C. BurleighAbstract:Small satellite Systems enable whole new class of missions for navigation, communications, remote sensing and scientific research for both civilian and military purposes. As individual spacecraft are limited by the size, mass and power constraints, mass-produced small satellites in large constellations or clusters could be useful in many science missions such as gravity mapping, tracking of forest fires, finding water resources, etc. Constellation of satellites provide improved spatial and temporal resolution of the target. Small satellite constellations contribute innovative applications by replacing a single asset with several very capable spacecraft which opens the door to new applications. With increasing levels of autonomy, there will be a need for remote communication networks to enable communication between spacecraft. These space based networks will need to configure and maintain dynamic routes, manage intermediate nodes, and reconfigure themselves to achieve mission objectives. Hence, inter-satellite communication is a key aspect when satellites fly in formation. In this paper, we present the various researches being conducted in the small satellite community for implementing inter-satellite communications based on the Open System Interconnection (OSI) model. This paper also reviews the various design parameters applicable to the first three layers of the OSI model, i.e., physical, data link and network layer. Based on the survey, we also present a comprehensive list of design parameters useful for achieving inter-satellite communications for multiple small satellite missions. Specific topics include proposed solutions for some of the challenges faced by small satellite Systems, enabling operations using a network of small satellites, and some examples of small satellite missions involving formation flying aspects.
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Survey of Inter-Satellite Communication for Small Satellite Systems: Physical Layer to Network Layer View
IEEE Communications Surveys & Tutorials, 2016Co-Authors: Radhika Radhakrishnan, William W. Edmonson, Fatemeh Afghah, Ramon Martinez Rodriguez-osorio, Frank Pinto, Scott C. BurleighAbstract:Small satellite Systems enable a whole new class of missions for navigation, communications, remote sensing, and scientific research for both civilian and military purposes. As individual spacecraft are limited by the size, mass, and power constraints, mass-produced small satellites in large constellations or clusters could be useful in many science missions such as gravity mapping, tracking of forest fires, finding water resources, etc. The proliferation of small satellites will enable a better understanding of the near-Earth environment and provide an efficient and economical means to access the space through the use of multi-satellite solution. Constellation of satellites provide improved spatial and temporal resolution of the target. Small satellite constellations contribute innovative applications by replacing a single asset with several very capable spacecraft, which opens the door to new applications. Future space missions are envisioned to become more complex and operate farther from Earth, and will need to support autonomous operations with minimal human intervention. With increasing levels of autonomy, there will be a need for remote communication networks to enable communication between spacecraft. These space-based networks will need to configure and maintain dynamic routes, manage intermediate nodes, and reconfigure themselves to achieve mission objectives. Hence, inter-satellite communication is a key aspect when satellites fly in formation. In this survey, we present the various research being conducted in the small satellite community for implementing inter-satellite communications based on the open System Interconnection (OSI) model. This survey also reviews the various design parameters applicable to the first three layers of the OSI model, i.e., physical, data link, and network layer. Based on the survey, we also present a comprehensive list of design parameters useful for achieving inter-satellite communications for multiple small satellite missions. Specific topics include proposed solutions for some of the challenges faced by small satellite Systems, enabling operations using a network of small satellites, and some examples of small satellite missions involving formation flying aspects.
D Davies - One of the best experts on this subject based on the ideXlab platform.
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An interim dynamic induction motor model for stability studies in the WSCC
2003 IEEE Power Engineering Society General Meeting (IEEE Cat. No.03CH37491), 2003Co-Authors: L Pereira, D Kosterev, P Mackin, D Davies, J M Undrill, Wenchun ZhuAbstract:Summary form only given. An "interim" composite load containing a static part and a dynamic part has been implemented in the WSCC. The static part of the load model is about 80% of the total load and comprises of existing static load data from the WSCC members. The dynamic part is a default induction motor model for approximately 20% of the total load. This composite model is used for all loads in the full-scale WSCC grid models that are the basis for System Interconnection studies. The model is designed primarily to capture the effects of dynamic induction motor loads for highly stressed north to south flow conditions during summer peaks in the WSCC.
-
an interim dynamic induction motor model for stability studies in the wscc
IEEE Transactions on Power Systems, 2002Co-Authors: L Pereira, D Kosterev, P Mackin, D Davies, J M UndrillAbstract:An "interim" composite load model containing a static part and a dynamic part has been implemented in the Western Systems Coordinating Council (WSCC). The static part of the load model is about 80% of the total load and comprises of existing static load data from the WSCC members. The dynamic part is a default induction motor model for approximately 20% of the total load. This composite model is used for all loads in the full-scale WSCC grid models that are the basis for System Interconnection studies. The model is designed primarily to capture the effects of dynamic induction motor loads for highly stressed north to south flow conditions during summer peaks in the WSCC.
