mirror of
https://github.com/PX4/PX4-Autopilot.git
synced 2026-06-01 02:55:07 +08:00
More example mixers; three different fixed-wing configurations for FMU.
This commit is contained in:
+4
-1
@@ -21,7 +21,10 @@ ROMFS_FSSPEC := $(SRCROOT)/scripts/rcS~init.d/rcS \
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$(SRCROOT)/scripts/rc.standalone~init.d/rc.standalone \
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$(SRCROOT)/scripts/rc.standalone~init.d/rc.standalone \
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$(SRCROOT)/scripts/rc.PX4IO~init.d/rc.PX4IO \
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$(SRCROOT)/scripts/rc.PX4IO~init.d/rc.PX4IO \
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$(SRCROOT)/scripts/rc.PX4IOAR~init.d/rc.PX4IOAR \
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$(SRCROOT)/scripts/rc.PX4IOAR~init.d/rc.PX4IOAR \
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$(SRCROOT)/mixers/FMU_delta.mix~mixers/FMU_delta.mix
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$(SRCROOT)/mixers/FMU_delta.mix~mixers/FMU_delta.mix \
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$(SRCROOT)/mixers/FMU_AERT.mix~mixers/FMU_AERT.mix \
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$(SRCROOT)/mixers/FMU_AET.mix~mixers/FMU_AET.mix \
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$(SRCROOT)/mixers/FMU_RET.mix~mixers/FMU_ERT.mix
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#
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#
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# Add the PX4IO firmware to the spec if someone has dropped it into the
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# Add the PX4IO firmware to the spec if someone has dropped it into the
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@@ -0,0 +1,64 @@
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Aileron/rudder/elevator/throttle mixer for PX4FMU
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==================================================
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This file defines mixers suirable for controlling a fixed wing aircraft with
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aileron, rudder, elevator and throttle controls using PX4FMU. The configuration
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assumes the aileron servo(s) are connected to PX4FMU servo output 0, the
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elevator to output 1, the rudder to output 2 and the throttle to output 3.
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Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0
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(roll), 1 (pitch) and 3 (thrust).
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Aileron mixer
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-------------
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Two scalers total (output, roll).
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This mixer assumes that the aileron servos are set up correctly mechanically;
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depending on the actual configuration it may be necessary to reverse the scaling
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factors (to reverse the servo movement) and adjust the offset, scaling and
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endpoints to suit.
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As there is only one output, if using two servos adjustments to compensate for
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differences between the servos must be made mechanically. To obtain the correct
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motion using a Y cable, the servos can be positioned reversed from one another.
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M: 2
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S: 0 0 10000 10000 0 -10000 10000
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S: 0 0 10000 10000 0 -10000 10000
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Elevator mixer
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------------
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Two scalers total (output, roll).
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This mixer assumes that the elevator servo is set up correctly mechanically;
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depending on the actual configuration it may be necessary to reverse the scaling
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factors (to reverse the servo movement) and adjust the offset, scaling and
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endpoints to suit.
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M: 2
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S: 0 0 10000 10000 0 -10000 10000
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S: 0 1 10000 10000 0 -10000 10000
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Rudder mixer
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------------
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Two scalers total (output, yaw).
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This mixer assumes that the rudder servo is set up correctly mechanically;
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depending on the actual configuration it may be necessary to reverse the scaling
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factors (to reverse the servo movement) and adjust the offset, scaling and
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endpoints to suit.
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M: 2
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S: 0 0 10000 10000 0 -10000 10000
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S: 0 2 10000 10000 0 -10000 10000
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Motor speed mixer
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-----------------
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Two scalers total (output, thrust).
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This mixer generates a full-range output (-1 to 1) from an input in the (0 - 1)
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range. Inputs below zero are treated as zero.
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M: 2
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S: 0 0 10000 10000 0 -10000 10000
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S: 0 3 0 20000 -10000 -10000 10000
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@@ -0,0 +1,60 @@
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Aileron/elevator/throttle mixer for PX4FMU
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==================================================
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This file defines mixers suirable for controlling a fixed wing aircraft with
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aileron, elevator and throttle controls using PX4FMU. The configuration assumes
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the aileron servo(s) are connected to PX4FMU servo output 0, the elevator to
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output 1 and the throttle to output 3.
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Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0
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(roll), 1 (pitch) and 3 (thrust).
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Aileron mixer
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-------------
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Two scalers total (output, roll).
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This mixer assumes that the aileron servos are set up correctly mechanically;
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depending on the actual configuration it may be necessary to reverse the scaling
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factors (to reverse the servo movement) and adjust the offset, scaling and
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endpoints to suit.
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As there is only one output, if using two servos adjustments to compensate for
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differences between the servos must be made mechanically. To obtain the correct
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motion using a Y cable, the servos can be positioned reversed from one another.
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Alternatively, output 2 could be used as a second aileron servo output with
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separate mixing.
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M: 2
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S: 0 0 10000 10000 0 -10000 10000
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S: 0 0 10000 10000 0 -10000 10000
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Elevator mixer
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------------
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Two scalers total (output, roll).
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This mixer assumes that the elevator servo is set up correctly mechanically;
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depending on the actual configuration it may be necessary to reverse the scaling
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factors (to reverse the servo movement) and adjust the offset, scaling and
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endpoints to suit.
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M: 2
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S: 0 0 10000 10000 0 -10000 10000
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S: 0 1 10000 10000 0 -10000 10000
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Output 2
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--------
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This mixer is empty.
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M: 0
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Motor speed mixer
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-----------------
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Two scalers total (output, thrust).
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This mixer generates a full-range output (-1 to 1) from an input in the (0 - 1)
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range. Inputs below zero are treated as zero.
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M: 2
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S: 0 0 10000 10000 0 -10000 10000
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S: 0 3 0 20000 -10000 -10000 10000
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@@ -0,0 +1,53 @@
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Rudder/elevator/throttle mixer for PX4FMU
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=========================================
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This file defines mixers suirable for controlling a fixed wing aircraft with
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rudder, elevator and throttle controls using PX4FMU. The configuration assumes
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the rudder servo is connected to PX4FMU servo output 0, the elevator to output 1
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and the throttle to output 3.
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Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0
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(roll), 1 (pitch) and 3 (thrust).
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Rudder mixer
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------------
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Two scalers total (output, roll).
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This mixer assumes that the rudder servo is set up correctly mechanically;
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depending on the actual configuration it may be necessary to reverse the scaling
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factors (to reverse the servo movement) and adjust the offset, scaling and
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endpoints to suit.
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M: 2
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S: 0 0 10000 10000 0 -10000 10000
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S: 0 0 10000 10000 0 -10000 10000
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Elevator mixer
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------------
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Two scalers total (output, roll).
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This mixer assumes that the elevator servo is set up correctly mechanically;
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depending on the actual configuration it may be necessary to reverse the scaling
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factors (to reverse the servo movement) and adjust the offset, scaling and
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endpoints to suit.
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M: 2
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S: 0 0 10000 10000 0 -10000 10000
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S: 0 1 10000 10000 0 -10000 10000
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Output 2
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--------
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This mixer is empty.
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M: 0
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Motor speed mixer
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-----------------
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Two scalers total (output, thrust).
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This mixer generates a full-range output (-1 to 1) from an input in the (0 - 1)
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range. Inputs below zero are treated as zero.
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M: 2
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S: 0 0 10000 10000 0 -10000 10000
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S: 0 3 0 20000 -10000 -10000 10000
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+10
-12
@@ -1,12 +1,10 @@
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Delta-wing mixer for PX4FMU
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Delta-wing mixer for PX4FMU
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===========================
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===========================
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Lines in this file that begin with a capital letter and a colon are interpreted
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This file defines mixers suitable for controlling a delta wing aircraft using
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as mixer commands. All other lines are ignored.
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PX4FMU. The configuration assumes the elevon servos are connected to PX4FMU
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servo outputs 0 and 1 and the motor speed control to output 3. Output 2 is
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This delta-wing mixer assumes the elevon servos are connected to PX4FMU servo
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assumed to be unused.
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outputs 0 and 1 and the motor speed control to output 2. Output 3 is assumed to
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be unused.
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Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0
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Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0
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(roll), 1 (pitch) and 3 (thrust).
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(roll), 1 (pitch) and 3 (thrust).
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@@ -33,6 +31,11 @@ S: 0 0 10000 10000 0 -10000 10000
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S: 0 0 5000 3000 0 -10000 10000
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S: 0 0 5000 3000 0 -10000 10000
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S: 0 1 -5000 -5000 0 -10000 10000
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S: 0 1 -5000 -5000 0 -10000 10000
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Output 2
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--------
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This mixer is empty.
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M: 0
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Motor speed mixer
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Motor speed mixer
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-----------------
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-----------------
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@@ -43,9 +46,4 @@ range. Inputs below zero are treated as zero.
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M: 2
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M: 2
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S: 0 0 10000 10000 0 -10000 10000
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S: 0 0 10000 10000 0 -10000 10000
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S: 0 2 0 20000 -10000 -10000 10000
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S: 0 3 0 20000 -10000 -10000 10000
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We leave the fourth mixer empty.
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M: 0
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