Corpus ID: 14737810

Gain Scheduled Automatic Flight Control Systems Design for a Light Commercial Helicopter Model

@inproceedings{Abdulhamitbilal2012GainSA,
  title={Gain Scheduled Automatic Flight Control Systems Design for a Light Commercial Helicopter Model},
  author={E. Abdulhamitbilal and E. Jafarov},
  year={2012}
}
In this paper, nonlinear rigid body dynamics for rotorcraft mathematical model is studied. A linearization of helicopter flight dynamics is evaluated. Automatic Flight Control System (AFCS) with gain scheduled LQ optimal control is designed based on look-up tables. Stability analyses are performed and results are illustrated graphically for open and closed-loop systems. As seen from results, LQ optimal control system pushes eigenvalues to left side of imaginary axis without excessive control… Expand
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ITU-Light Commercial Helicopter flight dynamics
  • stability analysis, and interconnected control systems design, ITU-Library, Istanbul
  • 2010
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