Flight Dynamics Modeling, Linearization & Control of an Unstable Aircraft @VDEngineering
Flight Dynamics Modeling, Linearization & Control of an Unstable Aircraft  @VDEngineering
Uploaded November 2019 | Updated September 2026, 1 hour ago
#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_sec/SEC.Accom.html

Thank you for your consideration

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Flight Dynamics Modeling, Linearization & Control of an Unstable Aircraft
VDEngineering |

Flight Dynamics Modeling, Linearization & Control of an Unstable Aircraft

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