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