Merge pull request #1172 from sjwilks/wingwing_mixer

Wing wing mixer
This commit is contained in:
Lorenz Meier 2014-07-11 21:54:23 +02:00
commit 66e840ebd7
2 changed files with 52 additions and 1 deletions

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@ -32,7 +32,7 @@ then
param set FW_THR_CRUISE 0.65
fi
set MIXER FMU_Q
set MIXER wingwing
# Provide ESC a constant 1000 us pulse
set PWM_OUTPUTS 4
set PWM_DISARMED 1000

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@ -0,0 +1,51 @@
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