Blade Components

R2026b
Model the structural dynamics of rotor blades, providing blade states and derivatives for use with force computation blocks

Model the structural dynamics of rotor blades in a rotor system by solving isolated or coupled blade equations of motion. These blocks provide individual blade states and derivatives for integration with force computation models in multirotor and helicopter simulations.

Blocks

Rigid Blade (Flap and Lag)Rigid Blade (Flap and Lag)Simulate flap and lag motion of rotor blades (Since R2026b)