Using bifurcation methods to aid nonlinear dynamic inversion control law design

Journal of Guidance, Control, and Dynamics

Volumn 21, Issue 4, 1998, Pages 632-638

  Littleboy, D M ^a,b   Smith, P R ^a,b  

^a DEFENCE SCIENCE AND TECHNOLOGY LABORATORY   (United Kingdom)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; ANGLE OF ATTACK INDICATORS; BIFURCATION (MATHEMATICS); CONTROL SYSTEM ANALYSIS; CONTROL SYSTEM SYNTHESIS; FLIGHT DYNAMICS; SYSTEM STABILITY;

NONLINEAR DYNAMIC INVERSION CONTROL LAW;

NONLINEAR CONTROL SYSTEMS;

EID: 0032122923     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4282     Document Type: Article

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