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airframes: add ThunderFly Auto-G2 autogyro (#14015)

sbg
Roman Dvořák 5 years ago committed by Beat Küng
parent
commit
497ab07daf
  1. 50
      ROMFS/px4fmu_common/init.d/airframes/17002_TF-AutoG2
  2. 1
      ROMFS/px4fmu_common/mixers/CMakeLists.txt
  3. 55
      ROMFS/px4fmu_common/mixers/TF-AutoG2.main.mix
  4. 1
      Tools/px4airframes/rcout.py
  5. 2
      Tools/px4airframes/srcparser.py

50
ROMFS/px4fmu_common/init.d/airframes/17002_TF-AutoG2

@ -0,0 +1,50 @@ @@ -0,0 +1,50 @@
#!/bin/sh
#
# @name ThunderFly Auto-G2
#
# @type Autogyro
# @class Autogyro
#
# @output MAIN1 rotor_head_L
# @output MAIN2 rotor_head_R
# @output MAIN3 elevator
# @output MAIN4 rudder
# @output MAIN5 rudder (second, optional)
# @output MAIN6 throttle
# @output MAIN7 wheel
#
# @output AUX1 feed-through of RC AUX1 channel for prerotator (optional)
# @output AUX2 feed-through of RC AUX2 channel for release device (optional)
#
# @url https://github.com/ThunderFly-aerospace/Auto-G2/
# @maintainer ThunderFly s.r.o., Roman Dvorak <dvorakroman@thunderfly.cz>
#
sh /etc/init.d/rc.fw_defaults
if [ $AUTOCNF = yes ]
then
param set BAT_CAPACITY 2500.0
param set BAT_N_CELLS 3
param set PWM_AUX_RATE 50
param set PWM_RATE 50
param set SENS_BOARD_ROT 8
param set FW_AIRSPD_MAX 20
param set FW_AIRSPD_MIN 7
param set FW_AIRSPD_TRIM 13
param set FW_THR_CRUISE 0.8
param set FW_MAN_P_MAX 25.0
param set FW_MAN_R_MAX 25.0
param set FW_PR_I 0.02
param set FW_R_LIM 40
param set FW_P_LIM_MAX 25.0
param set FW_P_LIM_MIN -5.0
param set FW_P_RMAX_NEG 20.0
fi
set MIXER TF-AutoG2
set MIXER_AUX pass

1
ROMFS/px4fmu_common/mixers/CMakeLists.txt

@ -84,4 +84,5 @@ px4_add_romfs_files( @@ -84,4 +84,5 @@ px4_add_romfs_files(
vtol_delta.aux.mix
wingwing.main.mix
zmr250.main.mix
TF-AutoG2.main.mix
)

55
ROMFS/px4fmu_common/mixers/TF-AutoG2.main.mix

@ -0,0 +1,55 @@ @@ -0,0 +1,55 @@
Aileron/rudder/elevator/throttle mixer for PX4FMU
==================================================
Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0
(roll), 1 (pitch) and 3 (thrust).
CH1, 2: rotor-head mixer
-------------
Two scalers total (output, roll).
M: 2
O: 10000 10000 0 -10000 10000
S: 0 0 -10000 -10000 0 -10000 10000
S: 0 1 10000 10000 0 -10000 10000
M: 2
O: 10000 10000 0 -10000 10000
S: 0 0 -10000 -10000 0 -10000 10000
S: 0 1 -10000 -10000 0 -10000 10000
CH3: Elevator, prerotator mixer
------------
Two scalers total (output, roll).
M: 1
O: 7500 7500 0 -10000 10000
S: 3 6 10000 10000 0 -10000 10000
CH4, 5: Rudder mixer
------------
Two scalers total (output, yaw).
M: 1
S: 0 2 10000 10000 0 -10000 10000
M: 1
S: 0 2 -10000 -10000 0 -10000 10000
CH4: Motor speed mixer
-----------------
Two scalers total (output, thrust).
M: 1
S: 0 3 0 20000 -10000 -10000 10000
CH3: Wheel mixer
------------
Two scalers total (output, yaw).
M: 1
S: 0 2 10000 10000 0 -10000 10000

1
Tools/px4airframes/rcout.py

@ -28,6 +28,7 @@ class RCOutput(): @@ -28,6 +28,7 @@ class RCOutput():
"# 12000 .. 12999 Octo Cox\n"
"# 13000 .. 13999 VTOL\n"
"# 14000 .. 14999 Tri Y\n"
"# 17000 .. 17999 Autogyro\n"
"\n")
result += "\n"
result += "set AIRFRAME none\n"

2
Tools/px4airframes/srcparser.py

@ -88,6 +88,8 @@ class ParameterGroup(object): @@ -88,6 +88,8 @@ class ParameterGroup(object):
return "YMinus"
elif (self.name == "Tricopter Y+"):
return "YPlus"
elif (self.name == "Autogyro"):
return "Autogyro"
elif (self.name == "Rover"):
return "Rover"
elif (self.name == "Boat"):

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