Adding a new Airframe Configuration
PX4 uses canned configurations as starting point for airframes. Adding a configuration is straightforward: Create a new file which is prepended with a free autostart ID in the init.d folder and build and upload the software.
Developers not wanting to create their own configuration can instead customize existing configurations using text files on the microSD card, as detailed on the custom system startup page.
An airframe configuration consists of three main blocks:
- The apps it should start, e.g. multicopter or fixed wing controllers
- The physical configuration of the system (e.g. a plane, wing or multicopter). This is called mixer.
- Tuning gains
These three aspects are mostly independent, which means that many configurations share the same physical layout of the airframe and start the same applications and most differ in their tuning gains.
A typical configuration file is below.
# # @name Wing Wing (aka Z-84) Flying Wing # # @url https://pixhawk.org/platforms/planes/z-84_wing_wing # # @type Flying Wing # # @output MAIN1 left aileron # @output MAIN2 right aileron # @output MAIN4 throttle # # @output AUX1 feed-through of RC AUX1 channel # @output AUX2 feed-through of RC AUX2 channel # @output AUX3 feed-through of RC AUX3 channel # # @maintainer Lorenz Meier <firstname.lastname@example.org> # sh /etc/init.d/rc.fw_defaults if [ $AUTOCNF == yes ] then param set BAT_N_CELLS 2 param set FW_AIRSPD_MAX 15 param set FW_AIRSPD_MIN 10 param set FW_AIRSPD_TRIM 13 param set FW_ATT_TC 0.3 param set FW_L1_DAMPING 0.74 param set FW_L1_PERIOD 16 param set FW_LND_ANG 15 param set FW_LND_FLALT 5 param set FW_LND_HHDIST 15 param set FW_LND_HVIRT 13 param set FW_LND_TLALT 5 param set FW_THR_LND_MAX 0 param set FW_PR_FF 0.35 param set FW_RR_FF 0.6 param set FW_RR_P 0.04 fi # Configure this as plane set MAV_TYPE 1 # Set mixer set MIXER wingwing # Provide ESC a constant 1000 us pulse set PWM_OUT 4 set PWM_DISARMED 1000
IMPORTANT REMARK: If you want to reverse a channel, never do this neither on your RC transmitter nor with e.g
RC1_REV. The channels are only reversed when flying in manual mode, when you switch in an autopilot flight mode, the channels output will still be wrong (it only inverts your RC signal). Thus for a correct channel assignment change either your PWM signals with
PWM_MAIN_REV1 (e.g. for channel one) or change the signs for both output scaling and output range in the corresponding mixer (see below).
A typical configuration file is below.
The plugs of the servos / motors go in the order of the mixers in this file.
So MAIN1 would be the left aileron, MAIN2 the right aileron, MAIN3 is empty (note the Z: zero mixer) and MAIN4 is throttle (to keep throttle on output 4 for common fixed wing configurations).
A mixer is encoded in normalized units from -10000 to 10000, corresponding to -1..+1.
M: 2 O: 10000 10000 0 -10000 10000 S: 0 0 -6000 -6000 0 -10000 10000 S: 0 1 6500 6500 0 -10000 10000
Where each number from left to right means:
- M: Indicates two scalers for two inputs
- O: Indicates the output scaling (1 in negative, 1 in positive), offset (zero here), and output range (-1..+1 here). If you want to invert your PWM signal, the signs for both output scalings and both output range numbers have to be changed. (
O: -10000 -10000 0 10000 -10000)
- S: Indicates the first input scaler: It takes input from control group #0 (attitude controls) and the first input (roll). It scales the input * 0.6 and reverts the sign (-0.6 becomes -6000 in scaled units). It applies no offset (0) and outputs to the full range (-1..+1)
- S: Indicates the second input scaler: It takes input from control group #0 (attitude controls) and the second input (pitch). It scales the input * 0.65 and reverts the sign (-0.65 becomes -6500 in scaled units). It applies no offset (0) and outputs to the full range (-1..+1)
Both scalers are added, which for a flying wing means the control surface takes maximum 60% deflection from roll and 65% deflection from pitch. As it is over-committed with 125% total deflection for maximum pitch and roll, it means the first channel (roll here) has priority over the second channel / scaler (pitch).
The complete mixer looks like this:
Delta-wing mixer for PX4FMU =========================== Designed for Wing Wing Z-84 This file defines mixers suitable for controlling a delta wing aircraft using PX4FMU. The configuration assumes the elevon servos are connected to PX4FMU servo outputs 0 and 1 and the motor speed control to output 3. Output 2 is assumed to be unused. Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0 (roll), 1 (pitch) and 3 (thrust). See the README for more information on the scaler format. Elevon mixers ------------- Three scalers total (output, roll, pitch). On the assumption that the two elevon servos are physically reversed, the pitch input is inverted between the two servos. The scaling factor for roll inputs is adjusted to implement differential travel for the elevons. M: 2 O: 10000 10000 0 -10000 10000 S: 0 0 -6000 -6000 0 -10000 10000 S: 0 1 6500 6500 0 -10000 10000 M: 2 O: 10000 10000 0 -10000 10000 S: 0 0 -6000 -6000 0 -10000 10000 S: 0 1 -6500 -6500 0 -10000 10000 Output 2 -------- This mixer is empty. Z: Motor speed mixer ----------------- Two scalers total (output, thrust). This mixer generates a full-range output (-1 to 1) from an input in the (0 - 1) range. Inputs below zero are treated as zero. M: 1 O: 10000 10000 0 -10000 10000 S: 0 3 0 20000 -10000 -10000 10000
Getting the new airframe to show in QGroundControl
The airframe meta data is bundled in the .px4 firmware file (which is a zipped JSON file).
Ensure to flash the resulting .px4 file in QGroundControl (custom file option) to load the meta data into the application. The new airframe will then be available in the user interface.