Wing rock suppression in the F-15 aircraft

22nd Atmospheric Flight Mechanics Conference

Volumn , Issue , 1997, Pages 640-652

  Liebst, Brad S ^a   DeWitt, Bruce R ^b  

^a AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; BIFURCATION (MATHEMATICS); CONTROL SURFACES; EIGENVALUES AND EIGENFUNCTIONS; FEEDBACK; ROCKS; SUPERSONIC AIRCRAFT;

AERODYNAMIC COEFFICIENTS; ANGLE OF ATTACKS (AOA); BIFURCATION THEORY; EIGEN-VALUE; FEEDBACK PARAMETERS; LINEAR FEEDBACK CONTROL; SENSITIVE PARAMETER; WING ROCK SUPPRESSION;

FIGHTER AIRCRAFT;

EID: 84982318687     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (18)

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