matlab codes for helicopter dynamics
ics(t, x, params, controls) % x: state vector [x; y; z; u; v; w; phi; theta; psi; p; q; r] % params: helicopter parameters % controls: control inputs % Extract states position = x(1:3); velocity = x(4:6); attitude = x(7:9); angular_velocity = x(10:12); % Compute forces