Propulsion

Simulate engine component, system, 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.

Blocks

Multirotor	Multirotor dynamics (Since R2023a)
Rotor	Rotor dynamics (Since R2023a)
Turbofan Engine System	Implement first-order representation of turbofan engine with controller

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Compute thrust and torque coefficient of an isolated rotor.

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