Development of a low-cost and versatile flight test platform

Journal of Aircraft

Volumn 34, Issue 1, 1997, Pages 9-19

  Campos, L M B C ^a,b   Fonseca, A A ^a   Azinheira, J R C ^a   Loura, J P ^a  

^a INSTITUTO SUPERIOR TÉCNICO   (Portugal)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT INSTRUMENTS; DAMPING; EQUATIONS OF MOTION; FLIGHT DYNAMICS; MATHEMATICAL MODELS; TEST FACILITIES;

AVIOCAR TWIN TURBOPROP LIGHT AIRPLANE CASA 212; FLIGHT TEST INSTRUMENTATION (FTI) SYSTEM; LINEAR LONGITUDINAL STABILITY MODELS; PHUGOID MODE; PROPELLER SLIPSTREAM EQUATIONS;

RESEARCH AIRCRAFT;

EID: 0030836279     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2154     Document Type: Article

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