Aircraft Control using Nonlinear Dynamic Inversion

Simulate the Nonlinear Dynamic Inversion Controller for the longitudinal dynamics of a small aircraft described by Stevens & Lewis (2003)
605 Downloads
Aktualisiert 12. Jul 2023

Lizenz anzeigen

Simulate the Nonlinear Dynamic Inversion Controller for the longitudinal dynamics of a small aircraft described by Stevens & Lewis (2003) pp 495-500 (also see Example problem 2.4-1, pp 140-141)
The code is based on the codes provided in Stevens & Lewis (2003), Figures 5.8-6 & 5.8-7.
We have tried to keep the same structure and variable names although these seem to be based on FORTRAN code.
Thus the code and structure could be improved. We have also corrected a few errors in the original code, particularly with the definition of C* which needs modifying to work with a nonlinear controller.

Zitieren als

B.L. Steven & F.L. Lewis (2003) "Aircraft Flight Control & Simulation", John Wiley (edition 2)

James Whidborne (2024). Aircraft Control using Nonlinear Dynamic Inversion (https://www.mathworks.com/matlabcentral/fileexchange/82199-aircraft-control-using-nonlinear-dynamic-inversion), MATLAB Central File Exchange. Abgerufen.

Kompatibilität der MATLAB-Version
Erstellt mit R2021b
Kompatibel mit allen Versionen
Plattform-Kompatibilität
Windows macOS Linux
Kategorien
Mehr zu GNC and Avionics finden Sie in Help Center und MATLAB Answers

Community Treasure Hunt

Find the treasures in MATLAB Central and discover how the community can help you!

Start Hunting!
Version Veröffentlicht Versionshinweise
1.03

more ghost code removed from function xdot=NonLinDynInv(x,u)

1.02

Code cleaned up to remove some "ghost code"

1.01

v 1.0 has a bug in main calling line 69 - now corrected

1.0.0