ROMFS: delete redundant wing mixers

- these are nearly identical with slightly different scaling and haven't been tested for years
This commit is contained in:
Daniel Agar 2021-07-13 13:32:05 -04:00 committed by Lorenz Meier
parent a8bf8d42db
commit ad11927661
10 changed files with 5 additions and 205 deletions

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@ -48,8 +48,7 @@ param set-default PWM_MAIN_DISARM 1000
# the payload bay is pitched up about 7 degrees
param set-default SENS_BOARD_Y_OFF 7
set MIXER phantom
set MIXER fw_generic_wing
# Provide ESC a constant 1000 us pulse
set PWM_OUT 4

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@ -48,7 +48,7 @@ param set-default PWM_MAIN_DISARM 1000
set MAV_TYPE 1
# Set mixer.
set MIXER wingwing
set MIXER fw_generic_wing
# Provide ESC a constant 1000 us pulse.
set PWM_OUT 4

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@ -27,5 +27,4 @@ param set-default FW_AIRSPD_TRIM 15
param set-default NAV_LOITER_RAD 150
set MIXER FX79
set MIXER fw_generic_wing

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@ -49,8 +49,7 @@ param set-default PWM_MAIN_DISARM 1000
# the payload bay is pitched up about 7 degrees
param set-default SENS_BOARD_Y_OFF 11.9
set MIXER phantom
set MIXER fw_generic_wing
# Provide ESC a constant 1000 us pulse
set PWM_OUT 4

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@ -63,6 +63,6 @@ param set-default PWM_MAIN_REV2 1
param set-default PWM_MAIN_MIN 900
param set-default PWM_MAIN_MAX 2100
set MIXER fw_generic_wing
set MIXER caipi
set PWM_OUT 1234

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@ -39,7 +39,6 @@ px4_add_romfs_files(
AETRFG.main.mix
babyshark.main.mix
blade130.main.mix
caipi.main.mix
CCPM.main.mix
claire.aux.mix
claire.main.mix
@ -53,7 +52,6 @@ px4_add_romfs_files(
firefly6.aux.mix
firefly6.main.mix
fw_generic_wing.main.mix
FX79.main.mix
generic_diff_rover.main.mix
hexa_cox.main.mix
hexa_+.main.mix
@ -66,7 +64,6 @@ px4_add_romfs_files(
octo_+.main.mix
octo_x.main.mix
pass.aux.mix
phantom.main.mix
quad_dc.main.mix
quad_h.main.mix
quad_+.main.mix
@ -94,5 +91,4 @@ px4_add_romfs_files(
vtol_convergence.main.mix
vtol_delta.aux.mix
vtol_tailsitter_duo.main.mix
wingwing.main.mix
)

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@ -1,52 +0,0 @@
FX-79 Delta-wing mixer for PX4FMU
=================================
# @board px4_fmu-v2 exclude
Designed for FX-79.
TODO (sjwilks): Add mixers for flaps.
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
S: 0 0 8500 8500 0 -10000 10000
S: 0 1 9500 9500 0 -10000 10000
M: 2
S: 0 0 8500 8500 0 -10000 10000
S: 0 1 -9500 -9500 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
S: 0 3 0 20000 -10000 -10000 10000

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@ -1,48 +0,0 @@
Delta-wing mixer
===========================
Designed for TBS Caipirinha
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
S: 0 0 8000 8000 0 -10000 10000
S: 0 1 9000 9000 0 -10000 10000
M: 2
S: 0 0 8000 8000 0 -10000 10000
S: 0 1 -9000 -9000 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
S: 0 3 0 20000 -10000 -10000 10000

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@ -1,45 +0,0 @@
Phantom FX-61 mixer
===================
This file defines mixers suitable for controlling a delta wing aircraft using
PX4/Pixhawk. The configuration assumes the elevon servos are connected to
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 are set so that pitch will have more travel than roll.
M: 2
S: 0 0 -6000 -6000 0 -10000 10000
S: 0 1 6500 6500 0 -10000 10000
M: 2
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
S: 0 3 0 20000 -10000 -10000 10000

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@ -1,48 +0,0 @@
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
S: 0 0 -6000 -6000 0 -10000 10000
S: 0 1 6500 6500 0 -10000 10000
M: 2
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
S: 0 3 0 20000 -10000 -10000 10000