Aircraft Control using Nonlinear Dynamic Inversion

Versione 1.03 (4,55 KB) da James Whidborne
Simulate the Nonlinear Dynamic Inversion Controller for the longitudinal dynamics of a small aircraft described by Stevens & Lewis (2003)
5.0
(2)
531 download
Aggiornato 12 lug 2023

Visualizza la licenza

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.

Cita come

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. Recuperato .

Compatibilità della release di MATLAB
Creato con R2021b
Compatibile con qualsiasi release
Compatibilità della piattaforma
Windows macOS Linux
Categorie
Scopri di più su GNC and Avionics in Help Center e MATLAB Answers

Community Treasure Hunt

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

Start Hunting!

Versione Pubblicato Note della release
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