nonlinearDynamics
Class: Aero.FixedWing
Namespace: Aero
Syntax
state_derivatives = nonlinearDynamics(aircraft,state)
Description
returns the column vector of state_derivatives
= nonlinearDynamics(aircraft
,state
)state_derivatives
of the fixed-wing aircraft
aircraft
from the initial state state
.
Input Arguments
Output Arguments
Examples
Limitations
When used with Simulink.LookupTable
objects, this method requires a
Simulink® license.
Version History
Introduced in R2021a