added albatross config and mixer

This commit is contained in:
Andreas Antener 2015-11-02 17:40:32 +01:00 committed by Roman
parent d97ead81aa
commit 5e4df86091
4 changed files with 142 additions and 5 deletions

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@ -5,10 +5,12 @@
# @type Standard Plane
#
# @output MAIN1 aileron
# @output MAIN2 elevator
# @output MAIN3 rudder
# @output MAIN4 throttle
# @output MAIN5 wheel
# @output MAIN2 aileron
# @output MAIN3 elevator
# @output MAIN4 rudder
# @output MAIN5 throttle
# @output MAIN6 wheel
# @output MAIN7 flaps
#
# @output AUX1 feed-through of RC AUX1 channel
# @output AUX2 feed-through of RC AUX2 channel
@ -39,7 +41,7 @@ then
param set PWM_DISARMED 1000
fi
set MIXER AERTWF
set MIXER AAERTWF
# use PWM parameters for throttle channel
set PWM_OUT 5

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@ -0,0 +1,51 @@
#!nsh
#
# @name Applied Aeronautics Albatross
#
# @type Standard Plane
#
# @output MAIN1 aileron right
# @output MAIN2 aileron left
# @output MAIN3 v-tail right
# @output MAIN4 v-tail left
# @output MAIN5 throttle
# @output MAIN6 wheel
# @output MAIN7 flaps right
# @output MAIN8 flaps left
#
# @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 Andreas Antener <andreas@uaventure.com>
#
sh /etc/init.d/rc.fw_defaults
if [ $AUTOCNF == yes ]
then
param set FW_AIRSPD_MIN 10
param set FW_AIRSPD_TRIM 15
param set FW_AIRSPD_MAX 20
param set FW_MAN_P_MAX 55
param set FW_MAN_R_MAX 55
param set FW_R_LIM 55
param set FW_WR_FF 0.2
param set FW_WR_I 0.2
param set FW_WR_IMAX 0.8
param set FW_WR_P 1
param set FW_W_RMAX 0
# set disarmed value for the ESC
param set PWM_DISARMED 1000
fi
set MIXER AAVVTWFF
# use PWM parameters for throttle channel
set PWM_OUT 5
set PWM_DISARMED p:PWM_DISARMED
set PWM_MIN p:PWM_MIN
set PWM_MAX p:PWM_MAX

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@ -0,0 +1,84 @@
Aileron/v-tail/throttle/wheel/flaps mixer for PX4FMU
=======================================================
This file defines mixers suitable for controlling a fixed wing aircraft with
aileron, v-tail (rudder, elevator), throttle, steerable wheel and flaps
using PX4FMU.
The configuration assumes the aileron servos are connected to PX4FMU servo
output 0 and 1, the tail servos to output 2 and 3, the throttle
to output 4, the wheel to output 5 and the flaps to output 6 and 7.
Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0
(roll), 1 (pitch), 2 (yaw) and 3 (thrust) 4 (flaps) 6 (flaperon).
Aileron mixer (roll + flaperon)
---------------------------------
This mixer assumes that the aileron servos are set up correctly mechanically;
depending on the actual configuration it may be necessary to reverse the scaling
factors (to reverse the servo movement) and adjust the offset, scaling and
endpoints to suit.
M: 2
O: 10000 10000 0 -10000 10000
S: 0 0 10000 10000 0 -10000 10000
S: 0 6 10000 10000 0 -10000 10000
M: 2
O: 10000 10000 0 -10000 10000
S: 0 0 10000 10000 0 -10000 10000
S: 0 6 -10000 -10000 0 -10000 10000
V-tail mixers
-------------
Three scalers total (output, roll, pitch).
On the assumption that the two tail servos are physically reversed, the pitch
input is inverted between the two servos.
M: 2
O: 10000 10000 0 -10000 10000
S: 0 2 -7000 -7000 0 -10000 10000
S: 0 1 -8000 -8000 0 -10000 10000
M: 2
O: 10000 10000 0 -10000 10000
S: 0 2 -7000 -7000 0 -10000 10000
S: 0 1 8000 8000 0 -10000 10000
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
Wheel mixer
------------
Two scalers total (output, yaw).
This mixer assumes that the wheel servo is set up correctly mechanically;
depending on the actual configuration it may be necessary to reverse the scaling
factors (to reverse the servo movement) and adjust the offset, scaling and
endpoints to suit.
M: 1
O: 10000 10000 0 -10000 10000
S: 0 2 -10000 -10000 0 -10000 10000
Flaps mixer
------------
Flap servos are physically reversed.
M: 1
O: 10000 10000 0 -10000 10000
S: 0 4 10000 5000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 4 -10000 -5000 0 -10000 10000