Stability of dynamic inversion control laws applied to nonlinear aircraft pitch-axis models

International Journal of Control

Volumn 63, Issue 1, 1996, Pages 1-25

  Morton, Blaise ^a   Enns, Dale ^a   Zhang, Bing Yu ^b,c  

^a HONEYWELL   (United States)

^b UNIVERSITY OF CINCINNATI   (United States)

^c UNIVERSITY OF MINNESOTA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; AIRCRAFT MODELS; CONTROL THEORY; EQUATIONS OF MOTION; INVERSE KINEMATICS; ROBUSTNESS (CONTROL SYSTEMS); STABILITY;

AIRCRAFT PITCH-AXIS MODELS; DYNAMIC INVERSION CONTROL LAWS;

NONLINEAR CONTROL SYSTEMS;

EID: 0029754194     PISSN: 00207179     EISSN: 13665820     Source Type: Journal    
DOI: 10.1080/00207179608921828     Document Type: Article

References (14)

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