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

AIAA Atmospheric Flight Mechanics Conference and Exhibit

Volumn , Issue , 2008, Pages

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

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b NASA DRYDEN FLIGHT RESEARCH CENTER   (United States)

^c Dynamic Systems and Control Branch   (United States)

^d Aerodynamics Branch   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

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

ACCURATE MODELING; EQUATION ERROR METHOD; ESTIMATED PARAMETER; OPERATIONAL FLIGHTS; OPTIMIZED EXCITATION; OUTPUT ERROR METHOD; REAL-TIME DYNAMIC MODEL; STABILITY AND CONTROL;

TIME DOMAIN ANALYSIS;

EID: 77958188622     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-6201     Document Type: Conference Paper

References (18)

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