Robustness analysis and reliable flight regime estimation of an integrated resilent control system for a transport aircraft

AIAA Guidance, Navigation and Control Conference and Exhibit

Volumn , Issue , 2008, Pages

  Shin, Jong Yeob ^a,c   Belcastro, Christine ^b,d  

^a NATIONAL INSTITUTE OF AEROSPACE   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c Robust and Adaptive Control   (United States)

^d Dynamic Systems and Control Branch   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC COEFFICIENTS; ANALYSIS METHOD; COMMAND SIGNAL; COMPUTATIONAL APPROACH; ENTIRE FLIGHT ENVELOPE; FLIGHT ENVELOPE; FLIGHT REGIME; FRACTIONAL TRANSFORMS; LONGITUDINAL DYNAMICS; MATRIX; MODELING SOFTWARES; MOMENT OF INERTIA; NASA LANGLEY RESEARCH CENTER; NON-LINEAR DYNAMICS; PARAMETER UNCERTAINTY; RECOVERY SYSTEMS; ROBUSTNESS ANALYSIS; STRUCTURED SINGULAR VALUE ANALYSIS; UNMODELED DYNAMICS; VALIDATION PROCESS; VARYING PARAMETERS;

AERODYNAMICS; AIRCRAFT CONTROL; ANGLE OF ATTACK INDICATORS; CLOSED LOOP SYSTEMS; FLIGHT CONTROL SYSTEMS; MULTIVARIABLE CONTROL SYSTEMS; NASA; NAVIGATION; REMOTE CONTROL; ROBUST CONTROL; ROBUSTNESS (CONTROL SYSTEMS); TRANSPORT AIRCRAFT; UNCERTAINTY ANALYSIS; VALUE ENGINEERING;

FLIGHT ENVELOPES;

EID: 78651076696     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (25)

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