]> git.mxchange.org Git - flightgear.git/blobdiff - src/FDM/UIUCModel/uiuc_map_ice.cpp
Harald JOHNSEN:
[flightgear.git] / src / FDM / UIUCModel / uiuc_map_ice.cpp
index 7045d3f2487dcd21d7dd92fe2be2a84aac222323..ae32f4806f3ccdb1a43e9133ea719a1fbd92ab1e 100644 (file)
 ----------------------------------------------------------------------
  
  HISTORY:      04/08/2000   initial release
+               --/--/2002   (RD) add SIS icing
 
 ----------------------------------------------------------------------
  
  AUTHOR(S):    Bipin Sehgal       <bsehgal@uiuc.edu>
                Jeff Scott         <jscott@mail.com>
+               Robert Deters      <rdeters@uiuc.edu>
  
 ----------------------------------------------------------------------
  
@@ -137,6 +139,39 @@ void uiuc_map_ice()
   ice_map["kCn_b3"]               =      kCn_b3_flag                ;
   ice_map["beta_probe_wing"]      =      beta_probe_wing_flag       ;
   ice_map["beta_probe_tail"]      =      beta_probe_tail_flag       ;
+  ice_map["bootTime"]             =      bootTime_flag              ;
+  ice_map["eta_wing_left_input"]  =      eta_wing_left_input_flag   ;
+  ice_map["eta_wing_right_input"] =      eta_wing_right_input_flag  ;
+  ice_map["eta_tail_input"]       =      eta_tail_input_flag        ;
+  ice_map["nonlin_ice_case"]      =      nonlin_ice_case_flag       ;
+  ice_map["eta_tail"]             =      eta_tail_flag              ;
+  ice_map["eta_wing_left"]        =      eta_wing_left_flag         ;
+  ice_map["eta_wing_right"]       =      eta_wing_right_flag        ;
+  ice_map["demo_eps_alpha_max"]   =      demo_eps_alpha_max_flag    ;
+  ice_map["demo_eps_pitch_max"]   =      demo_eps_pitch_max_flag    ;
+  ice_map["demo_eps_pitch_min"]   =      demo_eps_pitch_min_flag    ;
+  ice_map["demo_eps_roll_max"]    =      demo_eps_roll_max_flag     ;
+  ice_map["demo_eps_thrust_min"]  =      demo_eps_thrust_min_flag   ;
+  ice_map["demo_eps_flap_max"]    =      demo_eps_flap_max_flag     ;
+  ice_map["demo_eps_airspeed_max"]=      demo_eps_airspeed_max_flag ;
+  ice_map["demo_eps_airspeed_min"]=      demo_eps_airspeed_min_flag ;
+  ice_map["demo_boot_cycle_tail"] =      demo_boot_cycle_tail_flag  ;
+  ice_map["demo_boot_cycle_wing_left"]=  demo_boot_cycle_wing_left_flag;
+  ice_map["demo_boot_cycle_wing_right"]= demo_boot_cycle_wing_right_flag;  
+  ice_map["demo_eps_pitch_input"] =      demo_eps_pitch_input_flag  ; 
+  ice_map["tactilefadef"]         =      tactilefadef_flag          ;
+  ice_map["tactile_pitch"]        =      tactile_pitch_flag         ;
+  ice_map["demo_ap_pah_on"]       =      demo_ap_pah_on_flag        ;
+  ice_map["demo_ap_alh_on"]       =      demo_ap_alh_on_flag        ;
+  ice_map["demo_ap_rah_on"]       =      demo_ap_rah_on_flag        ;
+  ice_map["demo_ap_hh_on"]        =      demo_ap_hh_on_flag         ;
+  ice_map["demo_ap_Theta_ref_"]   =      demo_ap_Theta_ref_flag     ;
+  ice_map["demo_ap_alt_ref_"]     =      demo_ap_alt_ref_flag       ;
+  ice_map["demo_ap_Phi_ref_"]     =      demo_ap_Phi_ref_flag       ;
+  ice_map["demo_ap_Psi_ref_"]     =      demo_ap_Psi_ref_flag       ;
+  ice_map["demo_tactile"]         =      demo_tactile_flag          ;
+  ice_map["demo_ice_tail"]        =      demo_ice_tail_flag         ;
+  ice_map["demo_ice_left"]        =      demo_ice_left_flag         ;
+  ice_map["demo_ice_right"]       =      demo_ice_right_flag        ;
 }
-
 // end uiuc_map_ice.cpp