AUTOMATIC PUSHBACK FOR FLIGHTGEAR http://gitlab.com/mdanil/flightgear-autopush Version 2.0.1 Copyright (c) 2018 Autopush authors: Michael Danilov Joshua Davidson http://github.com/Octal450 Merspieler http://gitlab.com/merspieler Some of the code (c) FlightGear Distribute under the terms of GPLv2. This project aims to develop a generic pushback for JSBSim and YASim aircraft, with the following characteristics. 1. Do the pushback procedure automatically. 2. Scale to different aircraft with minimum changes to their logic. 3. Use no computer resources in flight. INSTALLATION Minimum FlightGear version: 2018.0 NOTE: these steps cover the minimal testing setup. To get the most realism out of Autopush, you will have to add logic aircraft-side as described in the last step. 1. Copy the autopush.config.xml.template into your aircraft directory and the Goldhofert.xml into /Models/Autopush/ 2. Set up the pushback logic. Add the following line under of your set.xml Rename autopush-config.xml.template to autopush-config.xml and edit the file as described below. Alternatively, you can copy the contents of autopush-config.xml.template to under of your set.xml and make these modifications there. Change the aliases to point to the following data: steer-cmd-norm nose wheel steering command norm yaw nose wheel steering output norm or angle (see below) chocks chocks command bool (or leave it until step 7) available pushback availability bool (or leave it until step 7) Replace the MULTIPLIER in yaw-mult with: max steering angle if yaw is norm 1.0 if yaw is degrees 57.3 if yaw is radians Replace PITCH with the pushback's pitch relative to aircraft. If your aircraft's ground pitch varies greatly, you can make an alias to property with calculated relative pitch. Replace MIN_RADIUS with the minimum allowed turning radius in m of the center of the aircraft during pushback procedure. NOTE: on some aircraft the turning radius is different for taxi and pushback. Please check the aircraft's literature. Replace STOP_DIST with the stopping distance in m from pushback speed. Add under of your set.xml: Nasal/Autopush/autopush.nas Nasal/Autopush/driver.nas Nasal/Autopush/dynarr.nas Nasal/Autopush/route.nas Add under of your set.xml: /sim/model/autopush/route/show /sim/model/autopush/route/show-wingtip 3. Connect the force to FDM. 3.a. JSBSim: 3.a.1. Add the following under of your JSBSim XML. FRONT-X FRONT-Y FRONT-Z 1.0 0.0 0.0 Replace FRONT-X, FRONT-Y, FRONT-Z with coordinates of your front bogey. 3.a.2. Add the following under of your set.xml. 3.b. YASim. Add the following under of your YASim xml. Replace FRONT-X, FRONT-Y, FRONT-Z with coordinates of your front bogey. 4. Add the pushback model to your Model XML: Pushback MODEL FRONT-X FRONT-Y FRONT-Z Replace FRONT-X, FRONT-Y, FRONT-Z with coordinates of your front bogey. Replace MODEL with one of the following file names: Autopush/Goldhofert.xml for Goldhofer towbarless pushback Edit the "SETTINGS" part in the beginning of the Goldhofert.xml to match your setup. 5. Add gui/dialogs/autopush.xml to your aircraft's menu (see FlightGear documentation for editing the menu). 6. If you have a bug tracker, please add a note, that autopush related bugs should be reported here: https://gitlab.com/mdanil/flightgear-autopush/issues 7. Launch the simulator and try Autopush. After making sure it works, complete the support by implementing some logic in your aircraft and connecting the rest of the interface. CAUTION. 1. Make sure to HAVE A BACK-UP COPY of your work. 2. If anything is not clear in the instruction below, do not guess -- contact the authors. 7.1. When pushback is connected ("/sim/model/autopush/connected"), nose wheel steering must actuate at different speed, depending on its rollspeed. The exact dependency is different per aircraft and used pushback visual, and for most aircraft the only way to find it is trial and error until it "looks right": - the input must be taken from pushback steering command norm (set by autopush-config.xml, default: "/controls/flight/rudder"); - the output must be written to pushback orientation in degrees, radians or norm (set by autopush-config.xml, default: "/gear/gear[0]/steering-norm"). 7.2. Set or alias (in autopush-config.xml) the availability property "/sim/model/autopush/available". It must be false if e.g. the aircraft is moving too fast, the front wheel is not touching the ground, the aircraft is damaged or is outside of an airport etc. 7.3. Make Autopush remove wheel chocks by setting the alias in autopush-config.xml to the chocks property. (default: "/controls/gear/wheel-chocks"). 7.4. Optionally, Autopush may be made visible in multiplayer by duplicating the properties used in its model.xml into some unused MP properties. See the list in https://sourceforge.net/p/flightgear/flightgear/ci/next/tree/src/MultiPlayer/multiplaymgr.cxx around line 215, and then using those properties in the "SETTINGS" part of Autopush model.xml. After making these changes check the Autopush model.xml's settings and make sure they match the setup. Launch the simulator and try Autopush. TUNING There should normally be no need to change the coefficients, because the inertia of different aircraft is already taken into account. But the gear setup may differ enough to require some tuning. If these settings are changed during simulation, they take effect after disconnecting and reconnecting the pushback. Pushback (/sim/model/autopush): Coefficient Unit Description K_p ((km/h)/s)/(km/h) Proportional coefficient of PID. Defines the start/stop throttle and immediate response to speed difference deltaV = V_set - V. F_p (km/h)/s Proportional clipping. K_i ((km/h)/s)/((km/h)*s) Integral coefficient of PID. Defines how fast the steady throttle is ramped during the push. F_i (km/h)/s Integral clipping. K_d -((km/h)/s)/((km/h)/s) Differential coefficient of PID. Stabilizes the approaching of steady throttle. F_d (km/h)/s Differential clipping. Pushback driver (/sim/model/autopush/driver): Coefficient Unit Description F_V km/h Max towing speed in auto mode. K_psi 1/deg Amount of steering per heading correction. F_psi 1/deg Max steering per heading correction. K_deltapsi -1/(deg/s) Amount of steering compensation per heading derivative. F_psi 1/(deg/s) Max amount of steering compensation per heading derivative.