Path: Airships/Simulation
% Aerodynamic forces and moments for an airship. All terms in body frame.
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Form:
g = AirshipAero( alpha, beta, x, d, qBar, control, flex, rho )
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Inputs
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alpha Angle of attack (rad)
beta Sideslip (rad)
x State
d Aerodynamic data
qBar Dynamic pressure
control Controls
flex Flexible states (not implemented)
rho Atmospheric density
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Outputs
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g .torque (3,1) Core torques
.force (3,1) Core forces
.modal (:,1) Modal forces
.inertia (3,3) Delta inertia due to aerodynamics
.mass (3,3) Delta mass matrix due to aerodynamics
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Common: Quaternion/QForm Math: Linear/Cross Math: Linear/Unit
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