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tumbili 2015-10-19 14:55:32 +02:00 committed by Roman
parent 0bd23dd7c5
commit 2a2e2a27d3
1 changed files with 6 additions and 6 deletions
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ROMFS/px4fmu_common/mixers/AERTW.main.mix
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@ -1,16 +1,16 @@
Aileron/rudder/elevator/throttle/wheel mixer for PX4FMU Aileron/rudder/elevator/throttle/wheel/flaps mixer for PX4FMU
======================================================= =======================================================
This file defines mixers suitable for controlling a fixed wing aircraft with This file defines mixers suitable for controlling a fixed wing aircraft with
aileron, rudder, elevator, throttle and steerable wheel controls using PX4FMU. aileron, rudder, elevator, throttle and steerable wheel controls using PX4FMU.
The configuration assumes the aileron servo(s) are connected to PX4FMU servo The configuration assumes the aileron servo(s) are connected to PX4FMU servo
output 0, the elevator to output 1, the rudder to output 2, the throttle output 0 and 1, the elevator to output 2, the rudder to output 3, the throttle
to output 3 and the wheel to output 4. to output 4 and the wheel to output 5.
Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0 Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0
(roll), 1 (pitch), 2 (yaw) and 3 (thrust). (roll), 1 (pitch), 2 (yaw) and 3 (thrust) 4 (flaps) 6 (flaperon).
Flaperon mixer (ailerons + flaps) Aileron mixer (roll + flaperon)
--------------------------------- ---------------------------------
This mixer assumes that the aileron servos are set up correctly mechanically; This mixer assumes that the aileron servos are set up correctly mechanically;
@ -79,7 +79,7 @@ O: 10000 10000 0 -10000 10000
S: 0 2 10000 10000 0 -10000 10000 S: 0 2 10000 10000 0 -10000 10000
Gimbal / flaps / payload mixer for last three channels, Flaps / gimbal / payload mixer for last three channels,
using the payload control group using the payload control group
----------------------------------------------------- -----------------------------------------------------