Identification of non-linear derivative models from Bo 105 flight test data

Aeronautical Journal

Volumn 102, Issue 1011, 1998, Pages 1-8

  Rohlfs, M ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

FLUTTER (AERODYNAMICS); MATHEMATICAL MODELS; PARAMETER ESTIMATION; TIME DOMAIN ANALYSIS;

NONLINEAR DERIVATIVE HELICOPTER MODELS;

HELICOPTERS;

EID: 0031651511     PISSN: 00019240     EISSN: None     Source Type: Trade Journal    
DOI: None     Document Type: Article

References (12)

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3. FU, K.-H. and KALETKA, J. Frequency-domain identification of Bo 105 derivative models with rotor degrees of freedom. 16th European Rotorcraft Forum, Glasgow, UK, 1990 and J Amer Heli Soc, January 1993, 38, (1).
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9. HAMEL, P.G. (Ed) Rotorcraft System Identification. AGARD-LS-178, October 1991.
10. HAMEL, P.G. (Ed) Rotorcraft System Identification. AGARD-AR-280, September 1991.
11. ROHLFS, M. Identifizierung von nichtlinearen Derivativ- modellen aus Flugversuchsdaten des Hubschraubers Bo105. DLR-IB 111-96/17, 1996.
12. LIESE, K. Die Anwendbarkeit einfacher Hubschraubermodelle für flugmechanische Untersuchungen. Dissertation, Institut für Flugmechanik, TU Braunschweig, 1989.