AAE 421 Flight Dynamics and Control Software
Dynamics and Control Software Description (.pdf)
The software below is built around a flat Earth aircraft simulation using Simulink for MATLAB 5.2. The equations of motion are twelth order.
Cessna182.m (contains all aircraft specific constants)
CessnaInitialize.m (run this first)
FlatEarth.mdl (run this second)
FlatEarthAnal.m (run this third)
aircraft.m (contains the differential and output equations)
The MATLAB software below does linear aircraft simulation and analysis using the approach of Jan Roskam. The equations of motion for both longitudinal motion and lateral-directional motion are forth order.
The software below is built around a elliptical Earth aircraft simulation using Simulink for MATLAB 5.2. The equations of motion are twelth order. These MATLAB programs use some of the routines given under the flat Earth section above.
E_CessnaInitialize.m (run this first)
E_Earth.mdl (run this second)
E_EarthAnal.m (run this third)
E_aircraft.m (contains the differential and output equations)
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