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)
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Mise à jour 12 juil. 2023

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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.

Citation pour cette source

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. Récupéré le .

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Créé avec R2021b
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Version Publié le Notes de version
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