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Utiliser RT-LAB TestFlight
 
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RT-LAB TestFlight


Liste des entrées et sorties

List of Inputs
Number Name Description
1 Column Column input,Corresponding to the elevator control surface.
2 Wheel Wheel input, corresponding to the ailerons control surfaces.
3 Pedal Pedal input, corresponding to the rudder control surface.
4 FlapSlatLever Flaps lever position. The positions are associated with flaps control surfaces angles.
5 FSpoilerLever Flight spoilers lever position. The positions are associated with flight spoilers control surfaces angles. These surfaces are not used in this model.
6 GearDown Sets the aircraft model's landing gear up or down.
7 TrimCmd Trim input, controlling the stabilizer control surface.
8 Throttle_LH Left throttle input controlling the left engine thrust.
9 Throttle_RH Right throttle input controlling the right engine thrust.
10 Wind_Switch Switch for the aircraft's wind and gusts model.
11 Wind_Dir Wind and gusts direction.
12 Wind_Speed Wind and gust speed.
13 Latitude_cmd Waypoints latitudes.
14 Longitude_cmd Waypoints longitudes.
15 Altitude_cmd Waypoints altitudes.
16 Speed_cmd Waypoints speeds.
17 Autopilot_Switch Switch for the aircraft's autopilot.

List of Outputs
Number Name Description
1 KIAS Indicated airspeed (kts).
2 Gamma Flight path angle (deg).
3 Beta Sideslip angle (deg).
4 Track Track angle (deg).
5 W_Speed Wind speed (kts).
6 W_Dir Wind direction, with north being 0 (deg).
7 Delta Throttle Difference between left throttle and right throttle; typically 0 at trim.
8 Thrust Total engine thrust (N).
9 Climb Rate of climb or descent (ft/min).
10 Mach Mach number.
11 Altitude_ft Pressure altitude (ft).
12 Phi Roll angle (deg).
13 Theta Pitch angle (deg).
14 Psi Yaw angle (deg.)
15 ThrottleLH Left throttle.
16 ThrottleRH Right throttle.
17 Alpha Angle of attack (deg).
18 Latitude (td negative-s).< (positive-N, Latitude>Latitude (positive-N, negative-S).
19 Longitude Longitude (positive-E, negative-W).
20 GeodeticHeight Distance between the aircraft and the earth center.
21 P Roll rate, in body axis (deg/s).
22 Q Pitch rate, in body axis (deg/s).
23 R Yaw rate, in body axis (deg/s).
24 Radar_Altitude Height above ground level (ft).
25 Ground_Speed Ground speed (kts).
26 North_vel North velocity (kts).
27 East_vel East velocity (kts).
28 Vertical_Vel Vertical velocity (ft/min).
29 ACC_longitudinal Longitudinal acceleration, in body axis (g).
30 ACC_lateral Lateral acceleration, in body axis (g).
31 Acc_normal Normal acceleration, in body axis (g).
32 TAS_dot Rate of change in true airspeed (kts/s).
33 B2E_1_1 Body axis to earth axis transformation matrix (element 1, 1).
34 B2E_1_2 Body axis to earth axis transformation matrix (element 1, 2).
35 B2E_1_3 Body axis to earth axis transformation matrix (element 1, 3).
36 B2E_2_1 Body axis to earth axis transformation matrix (element 2, 1).
37 B2E_2_2 Body axis to earth axis transformation matrix (element 2, 2).
38 B2E_2_3 Body axis to earth axis transformation matrix (element 2, 3).
39 B2E_3_1 Body axis to earth axis transformation matrix (element 3, 1).
40 B2E_3_2 Body axis to earth axis transformation matrix (element 3, 2).
41 B2E_3_3 Body axis to earth axis transformation matrix (element 3, 3).
42 Nx Longitudinal load factor (g).
43 Ny Lateral load factor (g).
44 Nz Normal load factor (g).
45 Wpt_Number Current target point, or waypoint (1 to 5).
46 Stabilizer Aircraft's stabilizer angle (deg).
47 OpSimInfo 3x1 vector output containing: Simulation status data