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.
Topik & Kata Kunci
Penulis (3)
B
Ben Messaoud Safinaz
B
Belkheiri Mohammed
B
Belkheiri Ahmed
Akses Cepat
Informasi Jurnal
- Tahun Terbit
- 2023
- Sumber Database
- DOAJ
- DOI
- 10.3390/engproc2023029003
- Akses
- Open Access ✓