Bifurcation analysis of a high incidence aircraft with nonlinear dynamic inversion control

22nd Atmospheric Flight Mechanics Conference

Volumn , Issue , 1997, Pages 629-639

  Littleboy, D M ^a   Smith, P R ^a  

^a DEFENCE SCIENCE AND TECHNOLOGY LABORATORY   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; BIFURCATION (MATHEMATICS); CONTROL THEORY; DYNAMICS; FIGHTER AIRCRAFT; FLIGHT ENVELOPES; LONGITUDINAL CONTROL; NONLINEAR ANALYSIS;

BIFURCATION ANALYSIS; BIFURCATION METHODS; CLOSED LOOP MODELS; HIGH ANGLES OF ATTACK; HIGH INCIDENCE RESEARCH MODEL; INCIDENCE ANGLES; NONLINEAR DYNAMIC INVERSION; UNDESIRABLE EFFECTS;

CONTROL SURFACES;

EID: 84982318243     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)

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13. Smith P. R., 'A Simplified Approach to Nonlinear Dynamic Inversion Based Flight Control', DRA Report (unpublished), March 1996.