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Norman, Patrick
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Modeling and Simulation Enabled UAV Electrical Power System Design

SAE International Journal of Aerospace

  • Journal Article
  • 2011-01-2645
Published 2011-10-18 by SAE International in United States
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Average-Value Diode Rectifier Modeling for Aerospace Applications

Published 2011-10-18 by SAE International in United States
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Impact of Engine Certification Standards on the Design Requirements of More-Electric Engine Electrical System Architectures

SAE International Journal of Aerospace

  • Journal Article
  • 2014-01-2119
Published 2014-09-16 by SAE International in United States
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A Method for the Evaluation of the Effectiveness of Turboelectric Distributed Propulsion Power System Architectures

SAE International Journal of Aerospace

  • Journal Article
  • 2014-01-2120
Published 2014-09-16 by SAE International in United States
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Impact of Converter Interface Type on the Protection Requirements for DC Aircraft Power Systems

SAE International Journal of Aerospace

  • Journal Article
  • 2012-01-2224
Published 2012-10-22 by SAE International in United States
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A Holistic Approach towards Optimizing Energy Storage Response during Network Faulted Conditions within an Aircraft Electrical Power System

SAE International Journal of Aerospace

  • Journal Article
  • 2012-01-2229
Published 2012-10-22 by SAE International in United States
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Parametric Average-Value Converter Modeling for Aerospace Applications

SAE International Journal of Aerospace

  • Journal Article
  • 2012-01-2156
Published 2012-10-22 by SAE International in United States
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Adaptive Protection Methods for Aircraft Applications

Published 2010-11-02 by SAE International in United States
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Modelling the Fault Behaviour of a Superconducting Turboelectric Distributed Propulsion Network

Published 2014-09-16 by SAE International in United States
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Turboelectric Distributed Propulsion Protection System Design Trades

Published 2014-09-16 by SAE International in United States
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