Bifurcation analysis of eigenstructure assignment control in a simple nonlinear aircraft model

Journal of Guidance, Control, and Dynamics

Volumn 21, Issue 5, 1998, Pages 792-798

  Gibson, L P ^a,b   Nichols, N K ^a   Littleboy, D M ^c  

^a UNIVERSITY OF READING   (United Kingdom)

^b AIAA   (United States)

^c DEFENCE SCIENCE AND TECHNOLOGY LABORATORY   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; BIFURCATION (MATHEMATICS); CLOSED LOOP CONTROL SYSTEMS; CONTROL SYSTEM ANALYSIS; CONTROL SYSTEM SYNTHESIS; EIGENVALUES AND EIGENFUNCTIONS; FEEDBACK CONTROL; LINEAR CONTROL SYSTEMS; MATHEMATICAL MODELS; ROBUSTNESS (CONTROL SYSTEMS); TIME VARYING CONTROL SYSTEMS;

EIGENSTRUCTURE ASSIGNMENT CONTROL;

NONLINEAR CONTROL SYSTEMS;

EID: 0032164995     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4308     Document Type: Article

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