End-to-End Differentiable Models and Optimization for Solid Rocket Powered Aircraft with Plume Radiant Emission
I developed and implemented a set of differentiable sub-models for predicting exhaust plume radiant emission for solid rocket motors using the AeroSandbox and CasADi design optimization frameworks. The model showed good agreement with experimental radiant emission data, and can be used to optimize the design of solid rocket powered aircraft.









