The CEDAR project - Commercial engine damage assessment and reconfiguration

Collection of Technical Papers - 2007 AIAA InfoTech at Aerospace Conference

Volumn 2, Issue , 2007, Pages 1003-1015

  Pisano, Alan D ^a,b   Rufleth, Bradley ^a,b  

^a GE AVIATION   (United States)

^b MS: 24064   (Iran)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT PROPULSION; CONTROL SYSTEM ANALYSIS; DAMAGE DETECTION; LINEAR PROGRAMMING; REAL TIME CONTROL; REGRESSION ANALYSIS;

COMMERCIAL ENGINES; CONTROL FUNCTIONS; CONTROL RECONFIGURATION CAPABILITY; DIGITAL PROPULSION CONTROLS (FADEC);

DIGITAL CONTROL SYSTEMS;

EID: 35648963665     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-2809     Document Type: Conference Paper

References (2)

1. Frankenberger and A. Pisano, "Survivable Engine Control Algorithm Development (SECAD)", 2002 IEEE Aerospace Conference Proceedings, March 2002.
2. Pisano, A., and Frankenberger, C., "The SECAD Project - Vulnerability Reduction via Propulsion Control Logic", 2006 IEEE Aerospace Conference Proceedings, March 2006.