RCAIDE.Library.Methods.Stability.Common.compute_dynamic_flight_modes

compute_dynamic_flight_modes

compute_dynamic_flight_modes(state, settings, vehicle)

This function follows the stability axis EOM derivation in Blakelock to return the vehicle’s dynamic modes and state space

Assumptions:

Linerarized Equations are used following the reference below

Source:

Automatic Control of Aircraft and Missiles by J. Blakelock Pg 23 and 117 Dynanmics of Flight Stability and Control by Bernard Edkin and Llyod Reid Chapter 5,

Inputs:

conditions.aerodynamics conditions.static_stability

Outputs:

conditions.dynamic_stability.LatModes conditions.dynamic_stability.LongModes

Properties Used:

N/A