Real-time dynamic modeling: Data information requirements and flight-test results

Journal of Aircraft

Volumn 46, Issue 6, 2009, Pages 1894-1905

  Morelli, Eugene A ^a,c   Smith, Mark S ^b,d  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c Dynamic Systems and Control Branch   (United States)

^d M S D 2033

Author keywords

[No Author keywords available]

Indexed keywords

ERRORS; FLIGHT CONTROL SYSTEMS; FLIGHT DYNAMICS; FLIGHT SIMULATORS; FREQUENCY DOMAIN ANALYSIS; INFORMATION MANAGEMENT; SUPERSONIC AIRCRAFT;

EQUATION ERROR METHOD; ESTIMATED PARAMETER; OPTIMIZED EXCITATION; OUTPUT ERROR METHOD; POST-FLIGHT ANALYSIS; REAL-TIME DYNAMIC MODEL; SPEED OF CONVERGENCE; STABILITY AND CONTROL;

TIME DOMAIN ANALYSIS;

EID: 73849114884     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.40764     Document Type: Article

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