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Volumn 4, Issue , 2002, Pages 4649-4651

Nonlinear model predictive control of an aircraft gas turbine engine

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; CONSTRAINT THEORY; CONTROL SYSTEM ANALYSIS; FEEDBACK CONTROL; GAS TURBINES; KALMAN FILTERING; MATHEMATICAL MODELS; PREDICTIVE CONTROL SYSTEMS; REAL TIME SYSTEMS; SENSORS; SPURIOUS SIGNAL NOISE; STATE ESTIMATION;

EID: 0242417099     PISSN: 01912216     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (59)

References (6)
  • 4
    • 84945981008 scopus 로고
    • A simplified real-time engine model for developing aeroengine control system
    • paper #92-3321
    • Shaoji, J., "A Simplified Real-Time Engine Model For Developing Aeroengine Control System," AIAA Conference, Nashville TN, paper #92-3321, 1992.
    • (1992) AIAA Conference, Nashville TN
    • Shaoji, J.1
  • 5
    • 0004285285 scopus 로고    scopus 로고
    • CRC Press, United States
    • Athans, M., The Control Handbook, CRC Press, United States, pp. 589-594, 1996.
    • (1996) The Control Handbook , pp. 589-594
    • Athans, M.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.