Fractal boundaries of basin of attraction of NewtonRaphson method in helicopter trim

Computers and Mathematics with Applications

Volumn 60, Issue 10, 2010, Pages 2834-2858

  Chandra Sekhar, D ^a   Ganguli, R ^a  

^a INDIAN INSTITUTE OF SCIENCE   (India)

Author keywords

Aeroelastic analysis; Fractals; Helicopter; NewtonRaphson method; System of nonlinear algebraic equations

Indexed keywords

AEROELASTIC ANALYSIS; ALGEBRAIC EQUATIONS; BASIN OF ATTRACTION; BASINS OF ATTRACTION; CENTER OF GRAVITY; COLLECTIVE PITCH; COMPUTATIONAL TIME; CONTROL INPUTS; CYCLIC PITCH; FRACTAL BOUNDARIES; FREE WAKE MODEL; HELICOPTER TRIM; INITIAL ESTIMATE; INITIAL GUESS; KEY PROBLEMS; LATERAL CYCLIC PITCHES; NEWTON-RAPHSON; NONLINEAR ALGEBRAIC EQUATIONS; NUMERICAL SOLUTION; PITCH CONTROL; TAIL ROTORS;

AEROELASTICITY; ALGEBRA; FRACTALS; LONGITUDINAL CONTROL; NONLINEAR ANALYSIS; NONLINEAR EQUATIONS;

HELICOPTER ROTORS;

EID: 78049314600     PISSN: 08981221     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.camwa.2010.09.040     Document Type: Article

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