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Propulsion

R2026b
Simulate engine component, system, rotors, and controller

Estimate and create inertia tensors. Calculate moments about center of gravity due to forces applied at a point. To implement a first-order representation of the engine and the controller, use a turbofan engine system. It computes the thrust and fuel flow at a specific throttle position, Mach number, and altitude. Compute the aerodynamic forces and moments generated by one or more rotating propellers or rotors in all three dimensions.

Blocks

Turbofan Engine System blockTurbofan Engine SystemImplement first-order representation of turbofan engine with controller

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