forked from Archive/PX4-Autopilot
Generic AETR and AERT airframes
Bixler converted to generic AERT
This commit is contained in:
parent
7600242c96
commit
e1c050df09
|
@ -0,0 +1,5 @@
|
|||
#!nsh
|
||||
|
||||
sh /etc/init.d/rc.fw_defaults
|
||||
|
||||
set MIXER AETR
|
|
@ -65,7 +65,7 @@ fi
|
|||
|
||||
if param compare SYS_AUTOSTART 2101 101
|
||||
then
|
||||
sh /etc/init.d/2101_hk_bixler
|
||||
sh /etc/init.d/2101_fw_AERT
|
||||
set MODE custom
|
||||
fi
|
||||
|
||||
|
@ -81,6 +81,12 @@ then
|
|||
set MODE custom
|
||||
fi
|
||||
|
||||
if param compare SYS_AUTOSTART 2104
|
||||
then
|
||||
sh /etc/init.d/2104_fw_AETR
|
||||
set MODE custom
|
||||
fi
|
||||
|
||||
#
|
||||
# Flying wing
|
||||
#
|
||||
|
|
|
@ -0,0 +1,84 @@
|
|||
Aileron/Elevator/Throttle/Rudder mixer for PX4FMU
|
||||
==================================================
|
||||
|
||||
This file defines mixers suitable for controlling a fixed wing aircraft with
|
||||
aileron, rudder, elevator and throttle controls using PX4FMU. The configuration
|
||||
assumes the aileron servo(s) are connected to PX4FMU servo output 0, the
|
||||
elevator to output 1, the throttle to output 2 and the rudder to output 3.
|
||||
|
||||
Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0
|
||||
(roll), 1 (pitch) and 3 (thrust).
|
||||
|
||||
Aileron mixer
|
||||
-------------
|
||||
Two scalers total (output, roll).
|
||||
|
||||
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.
|
||||
|
||||
As there is only one output, if using two servos adjustments to compensate for
|
||||
differences between the servos must be made mechanically. To obtain the correct
|
||||
motion using a Y cable, the servos can be positioned reversed from one another.
|
||||
|
||||
M: 1
|
||||
O: 10000 10000 0 -10000 10000
|
||||
S: 0 0 10000 10000 0 -10000 10000
|
||||
|
||||
Elevator mixer
|
||||
------------
|
||||
Two scalers total (output, roll).
|
||||
|
||||
This mixer assumes that the elevator 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 1 -10000 -10000 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
|
||||
|
||||
Rudder mixer
|
||||
------------
|
||||
Two scalers total (output, yaw).
|
||||
|
||||
This mixer assumes that the rudder 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
|
||||
|
||||
Gimbal / flaps / payload mixer for last four channels,
|
||||
using the payload control group
|
||||
-----------------------------------------------------
|
||||
|
||||
M: 1
|
||||
O: 10000 10000 0 -10000 10000
|
||||
S: 2 0 10000 10000 0 -10000 10000
|
||||
|
||||
M: 1
|
||||
O: 10000 10000 0 -10000 10000
|
||||
S: 2 1 10000 10000 0 -10000 10000
|
||||
|
||||
M: 1
|
||||
O: 10000 10000 0 -10000 10000
|
||||
S: 2 2 10000 10000 0 -10000 10000
|
||||
|
||||
M: 1
|
||||
O: 10000 10000 0 -10000 10000
|
||||
S: 2 3 10000 10000 0 -10000 10000
|
Loading…
Reference in New Issue