Simulink Toolbox for the Modeling and Analysis of Thermodynamic Systems, such as gas turbines
Design and analyze low-thrust orbit transfers
NASA HL-20 Lifting Body Airframe Modeled with Simulink and Aerospace Blockset.
orbital transfer using solar-electric propulsion
Fully vectorized n-body equations of motion in second and first order form, along with C MEX implementations of an RKN 12-10 integrator.
PDF document and MATLAB script that demonstrates using Cowell’s method to predict orbital motion.
Tools for simple estimation of aircraft propulsion performance.
A simulation of a rocket that's pushed by wind resistance and must use jet propulsion to correct.
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