Flight Dynamics Modeling, Linearization & Control of an Unstable Aircraft
#SimulinkChallenge2019 #Matlab #Flight
My entry to the Simulink Student Challenge 2019
Longitudinal Nonlinear Flight Dynamics and Control of an unstable Fighter Aircraft.
The equations of motion, stability derivatives, aerodynamic coefficients for a longitudinal motion of an aircraft are all computed using Simulink which provides quick turnaround time.
A linearized MIMO state space model is then developed using PID Loops to control both speed and pitch angle simultaneously
Source:
https://dept.aem.umn.edu/~balas/darpa...
Thank you for your consideration
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