Interpretable Aeroelastic Models for Control at Insect Scale

I have separated the upper curve into individual contributions from angle of attack, angular velocity, angular acceleration, and remaining transients and bending in the C matrix. The coefficients of lift show that all of these contributions are important in deformation. The speed bump curve represents the contribution to deformation from angle of attack, while the green curve represents bending modes and transients, which are also significant. This information will be useful for designing control objectives, as deformation mainly tracks angle of attack rather than acceleration. This unexpected result will help us in utilizing this data effectively.