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Volumn , Issue 538 CP, 2008, Pages 661-665

Stability assessment of distributed Dc power systems for 'more- electric' aircraft

Author keywords

'more electric' aircraft; DC power systems; Power system stability

Indexed keywords

'MORE ELECTRIC' AIRCRAFT; CIRCUIT LAWS; COMPLETE SYSTEM; DC POWER SYSTEMS; EIGENVALUE ANALYSIS; EIGENVALUES; NONLINEAR STATE; OPERATING CONDITION; POWER SYSTEM STABILITY; SMALL SIGNAL STABILITY; STABILITY ASSESSMENT; SUB-SYSTEM; SUB-SYSTEMS; TIME-DOMAIN SIMULATIONS;

EID: 67449104477     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1049/cp:20080604     Document Type: Conference Paper
Times cited : (8)

References (14)
  • 1
    • 85072485446 scopus 로고    scopus 로고
    • On the concept of negative impedance instability in more electric aircraft power systems with constant power loads
    • 1999-01-2545
    • A. Emadi, B. Fahimi, and M. Ehsani, "On the concept of negative impedance instability in more electric aircraft power systems with constant power loads", SAE Journal, 1999-01-2545.
    • SAE Journal
    • Emadi, A.1    Fahimi, B.2    Ehsani, M.3
  • 2
    • 51049100337 scopus 로고    scopus 로고
    • Small signal stability studies of a 270V DC more electric aircraft power system
    • Dublin, 4-6 April
    • L. Han, J. Wang, and D. Howe, "Small signal stability studies of a 270V DC more electric aircraft power system", Proc. IEE PEMD2006, Dublin, pp. 197-201, 4-6 April, 2006.
    • (2006) Proc. IEE PEMD2006 , pp. 197-201
    • Han, L.1    Wang, J.2    Howe, D.3
  • 3
    • 0033681057 scopus 로고    scopus 로고
    • Negative impedance stabilising controls for PWM DC/DC converters using feedback linearization techniques
    • A. Emadi, and M. Ehsani, "Negative impedance stabilising controls for PWM DC/DC converters using feedback linearization techniques", Proc. IECECE2000, pp. 613-620.
    • Proc. IECECE2000 , pp. 613-620
    • Emadi, A.1    Ehsani, M.2
  • 7
    • 67449100762 scopus 로고    scopus 로고
    • Experimental testing of a 250 kW fault-tolerant permanent magnet power generation system for large civil aeroengines
    • in press
    • Z. Sun, J. D. Ede, J. Wang, G. W. Jewell, J. Cullen and A. Mitcham, "Experimental testing of a 250 kW fault-tolerant permanent magnet power generation system for large civil aeroengines", AIAA Journal of propulsion and power, in press.
    • AIAA Journal of Propulsion and Power
    • Sun, Z.1    Ede, J.D.2    Wang, J.3    Jewell, G.W.4    Cullen, J.5    Mitcham, A.6
  • 12
    • 0031369796 scopus 로고    scopus 로고
    • Electromechanical actuator for a transport aircraft spoiler surface
    • G. Fronista and G. Bradbury, "Electromechanical actuator for a transport aircraft spoiler surface", Energy Conversion Engineering Conference, IECEC-97, Vol.1(27), pp. 694-698, 1999.
    • (1999) Energy Conversion Engineering Conference, IECEC-97 , vol.1 , Issue.27 , pp. 694-698
    • Fronista, G.1    Bradbury, G.2
  • 13
    • 0036038019 scopus 로고    scopus 로고
    • The more electric aero-engine: A general overview from an engine manufacturer
    • M. Provost, "The more electric aero-engine: A general overview from an engine manufacturer", Power Electronics, Machines and Drives (PEMD) Conference, pp. 246-251, 2002.
    • (2002) Power Electronics, Machines and Drives (PEMD) Conference , pp. 246-251
    • Provost, M.1
  • 14
    • 84868989806 scopus 로고    scopus 로고
    • E-Flight Airbus 320
    • www.e-flight.com/a320.htm, E-Flight Airbus 320.


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.