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Volumn 47, Issue 3, 2002, Pages 198-208

An experimental evaluation of generalized predictive control for tiltrotor aeroelastic stability augmentation in airplane mode of flight

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; ALGORITHMS; DIFFERENCE EQUATIONS; LINEAR EQUATIONS; MILITARY AIRCRAFT; PREDICTIVE CONTROL SYSTEMS; TIME DOMAIN ANALYSIS; WIND TUNNELS;

EID: 0036640921     PISSN: 00028711     EISSN: None     Source Type: Journal    
DOI: 10.4050/jahs.47.198     Document Type: Article
Times cited : (32)

References (33)
  • 6
    • 0005868145 scopus 로고
    • Dynamics of tilting proprotor aircraft in cruise flight
    • May
    • (1974) NASA TN , vol.D-7677
    • Johnson, W.1
  • 23
    • 0005857133 scopus 로고    scopus 로고
    • State-space system realization with input- and output-data correlation
    • April
    • (1997) NASA TP , vol.3622
    • Juang, J.-N.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.