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A Direct Torque-Controlled Induction Machine Bidirectional Power Architecture for More Electric Aircraft

Journal Article
2009-01-3219
ISSN: 1946-3855, e-ISSN: 1946-3901
DOI: https://doi.org/10.4271/2009-01-3219
Published November 10, 2009 by SAE International in United States
A Direct Torque-Controlled Induction Machine Bidirectional Power Architecture for More Electric Aircraft
Sector:
Citation: O'Connell, T., Wells, J., Lamm, P., and DeWitt, L., "A Direct Torque-Controlled Induction Machine Bidirectional Power Architecture for More Electric Aircraft," SAE Int. J. Aerosp. 3(1):65-73, 2010, https://doi.org/10.4271/2009-01-3219.
Language: English

References

  1. Wells J. R. et al “Electrical accumulator unit for the energy optimized aircraft,” SAE International Journal of Aerospace 1 1071 1077 April 2009
  2. Depenbrock M. “Direct self-control (DSC) of inverter-fed induction machine,” IEEE Transactions on Power Electronics 3 420 429 Oct. 1988
  3. Noguchi T. Takahashi I. “A new quick-response and high-efficiency control strategy of an induction motor,” IEEE Transactions on Industry Applications 22 820 827 Sept./Oct. 1986
  4. Vas P. Sensorless Vector and Direct Torque Control Oxford, U. K. Oxford Univ. Press 1998
  5. Krause P. Wasynczuk O. Sudhoff S. Analysis of Electric Machinery and Drive Systems 2nd Piscataway, NJ IEEE Press 2002
  6. Amrhein M. Krein P.T. Fierro B.I. “Evaluation of a re-rated induction machine,” Proc. IEEE International Conference on Electric Machines and Drives (IEMDC '05) 1400 1407 May 2005

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