Hybrid Damage Adaptive Flight Controlwith Model Inversion Adaptation

نویسندگان

  • Nhan Nguyen
  • Kalmanje Krishnakumar
چکیده

This paper presents a hybrid neural net adaptive control method for damaged aircraft. The hybrid method utilizes an adaptive scheme that adjusts a dynamic inversion control model to account for damaged plant dynamics. The model inversion adaptive scheme is based on two approaches: 1) an indirect adaptive law based on the Lyapunov theory, and 2) a recursive least squares method for parameter estimation of damaged plant dynamics. Simulations show that the hybrid adaptive control can provide a significant improvement in the tracking performance over the direct adaptive control. Copyright c © 2007 IFAC

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تاریخ انتشار 2007