DOAJ Open Access 2023

Observer Backstepping Design for Flight Control

Ben Messaoud Safinaz Belkheiri Mohammed Belkheiri Ahmed

Abstrak

This paper presents observer backstepping as a new nonlinear flight control design framework. Flight control laws for general-purpose maneuvering in the presence of nonlinear lift and side forces are designed. The controlled variables are the angle of attack, the sideslip angle, and the roll rate. The stability has been proved using Lyapunov stability criteria. Control laws were evaluated using realistic aircraft simulation models, with highly encouraging results.

Penulis (3)

B

Ben Messaoud Safinaz

B

Belkheiri Mohammed

B

Belkheiri Ahmed

Format Sitasi

Safinaz, B.M., Mohammed, B., Ahmed, B. (2023). Observer Backstepping Design for Flight Control. https://doi.org/10.3390/engproc2023029003

Akses Cepat

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Informasi Jurnal
Tahun Terbit
2023
Sumber Database
DOAJ
DOI
10.3390/engproc2023029003
Akses
Open Access ✓