Function File: sys = WestlandLynx ()

Model of the Westland Lynx Helicopter about hover.

INPUTS
main rotor collective
longitudinal cyclic
lateral cyclic
tail rotor collective
STATES
pitch attitude           theta       [rad]
roll attitude            phi         [rad]
roll rate (body-axis)    p           [rad/s]
pitch rate (body-axis)   q           [rad/s]
yaw rate                 xi          [rad/s]
forward velocity         v_x         [ft/s]
lateral velocity         v_y         [ft/s]
vertical velocity        v_z         [ft/s]
OUTPUTS
heave velocity           H_dot       [ft/s]
pitch attitude           theta       [rad]
roll attitude            phi         [rad]
heading rate             psi_dot     [rad/s]
roll rate                p           [rad/s]
pitch rate               q           [rad/s]

References
[1] Skogestad, S. and Postlethwaite I. (2005) Multivariable Feedback Control: Analysis and Design: Second Edition. Wiley. http://www.nt.ntnu.no/users/skoge/book/2nd_edition/matlab_m/matfiles.html

Package: control