px4-firmware/ROMFS/px4fmu_common/mixers
Lorenz Meier e43625cfc1 ROMFS: Clear out SITL mixers from deployed image, delete unused mixers, move test mixers to test config 2016-07-01 18:08:32 +02:00
..
AAERTWF.main.mix added albatross config and mixer 2015-11-17 22:28:09 +01:00
AAVVTWFF.main.mix fixed flaps offset to have correct neutral position 2015-11-17 22:28:09 +01:00
AERT.main.mix Clean up mixers, remove unused pass-through mixers from planes clobbering up RAM 2016-03-12 16:43:30 +01:00
AET.main.mix Clean up mixers, remove unused pass-through mixers from planes clobbering up RAM 2016-03-12 16:43:30 +01:00
AETR.main.mix Clean up mixers, remove unused pass-through mixers from planes clobbering up RAM 2016-03-12 16:43:30 +01:00
CCPM.main.mix Changed naming of the mixers to get rid of umbiguity as outputs are actually going to be driven by io, not fmu 2015-01-08 00:53:52 +02:00
FMU_pass.mix Merge working changes into export-build branch. 2013-04-26 16:14:32 -07:00
FX79.main.mix romfs mixer files: remove executable bit of file permission 2016-04-11 11:23:00 +02:00
IO_pass.main.mix renamed IO_pass.mix to IO_pass.main.mix 2015-02-20 14:42:29 +01:00
IO_pass.mix created copy of IO_pass.mix -> IO_pass.main.mix 2015-02-20 15:16:25 +01:00
Q.main.mix Clean up mixers, remove unused pass-through mixers from planes clobbering up RAM 2016-03-12 16:43:30 +01:00
README.md fix mixers README.md 2015-06-07 21:37:07 -04:00
RET.main.mix Clean up mixers, remove unused pass-through mixers from planes clobbering up RAM 2016-03-12 16:43:30 +01:00
Viper.main.mix romfs mixer files: remove executable bit of file permission 2016-04-11 11:23:00 +02:00
X5.main.mix Clean up mixers, remove unused pass-through mixers from planes clobbering up RAM 2016-03-12 16:43:30 +01:00
caipi.main.mix Caipi: Fix mixer and reverse params 2015-06-08 14:45:48 +02:00
caipirinha_vtol.main.mix reduce output scaling as workaround for broken output limits 2016-03-01 09:21:58 +01:00
claire.aux.mix Quad tilt vtol config (#4473) 2016-06-29 09:14:18 +02:00
claire.main.mix Quad tilt vtol config (#4473) 2016-06-29 09:14:18 +02:00
coax.main.mix Added configuration file for coaxial helicopter 2015-12-05 10:40:34 +01:00
delta.main.mix Clean up mixers, remove unused pass-through mixers from planes clobbering up RAM 2016-03-12 16:43:30 +01:00
easystar.main.mix Changed naming of the mixers to get rid of umbiguity as outputs are actually going to be driven by io, not fmu 2015-01-08 00:53:52 +02:00
firefly6.aux.mix Bring back the ability to transition plus a partial cleanup of tiltrotor support and firefly6 config updates. 2015-08-05 16:16:03 +02:00
firefly6.main.mix Changed naming of the mixers to get rid of umbiguity as outputs are actually going to be driven by io, not fmu 2015-01-08 00:53:52 +02:00
hexa_+.main.mix Changed naming of the mixers to get rid of umbiguity as outputs are actually going to be driven by io, not fmu 2015-01-08 00:53:52 +02:00
hexa_cox.main.mix Changed naming of the mixers to get rid of umbiguity as outputs are actually going to be driven by io, not fmu 2015-01-08 00:53:52 +02:00
hexa_x.main.mix Changed naming of the mixers to get rid of umbiguity as outputs are actually going to be driven by io, not fmu 2015-01-08 00:53:52 +02:00
octo_+.main.mix Changed naming of the mixers to get rid of umbiguity as outputs are actually going to be driven by io, not fmu 2015-01-08 00:53:52 +02:00
octo_cox.main.mix Changed naming of the mixers to get rid of umbiguity as outputs are actually going to be driven by io, not fmu 2015-01-08 00:53:52 +02:00
octo_cox_w.main.mix Add Steadidrone MAVRIK mixer and gains. 2016-02-02 08:31:08 +01:00
octo_x.main.mix Changed naming of the mixers to get rid of umbiguity as outputs are actually going to be driven by io, not fmu 2015-01-08 00:53:52 +02:00
pass.aux.mix TBS Disco config: Enable manual pass-through 2015-05-04 13:02:29 +02:00
phantom.main.mix Clean up mixers, remove unused pass-through mixers from planes clobbering up RAM 2016-03-12 16:43:30 +01:00
quad_+.main.mix Quad mixers: Add AUX1-2 passthrough 2016-05-01 16:24:52 +02:00
quad_+_vtol.main.mix Fix typo for Quad + mixer 2015-07-30 15:59:42 +02:00
quad_h.main.mix Quad mixers: Add AUX1-2 passthrough 2016-05-01 16:24:52 +02:00
quad_w.main.mix Quad mixers: Add AUX1-2 passthrough 2016-05-01 16:24:52 +02:00
quad_x.main.mix Quad mixers: Add AUX1-2 passthrough 2016-05-01 16:24:52 +02:00
quad_x_vtol.main.mix Get closer to correct tailsitter mixer, still incomplete 2016-06-17 22:44:42 +02:00
sk450_deadcat.aux.mix Fixed comments 2015-03-06 18:57:38 -08:00
sk450_deadcat.main.mix Quad mixers: Add AUX1-2 passthrough 2016-05-01 16:24:52 +02:00
skywalker.main.mix Changed naming of the mixers to get rid of umbiguity as outputs are actually going to be driven by io, not fmu 2015-01-08 00:53:52 +02:00
tri_y_yaw+.main.mix tricopter comment polish 2015-02-06 19:04:51 -08:00
tri_y_yaw-.main.mix tricopter comment polish 2015-02-06 19:04:51 -08:00
vtol_AAERT.aux.mix Don't use the control surface abbreviation but use the actual channel assignment. 2015-08-06 10:49:39 +02:00
vtol_AAVVT.aux.mix Added V-Tail VTOL config and mixer 2015-11-19 04:56:33 +01:00
vtol_delta.aux.mix vtol delta quad plane: adjusted mixer scaling 2016-06-29 13:28:58 +02:00
vtol_quad_x.main.mix Add support for a 'standard' VTOL with pusher/tractor motor. 2015-08-06 10:49:39 +02:00
wingwing.main.mix Changed naming of the mixers to get rid of umbiguity as outputs are actually going to be driven by io, not fmu 2015-01-08 00:53:52 +02:00

README.md

PX4 mixer definitions

Files in this directory implement example mixers that can be used as a basis for customisation, or for general testing purposes.

For a detailed description of the mixing architecture and examples see: http://px4.io/dev/mixing

Syntax

Mixer definitions are text files; lines beginning with a single capital letter followed by a colon are significant. All other lines are ignored, meaning that explanatory text can be freely mixed with the definitions.

Each file may define more than one mixer; the allocation of mixers to actuators is specific to the device reading the mixer definition, and the number of actuator outputs generated by a mixer is specific to the mixer.

For example: each simple or null mixer is assigned to outputs 1 to x in the order they appear in the mixer file.

A mixer begins with a line of the form

<tag>: <mixer arguments>

The tag selects the mixer type; 'M' for a simple summing mixer, 'R' for a multirotor mixer, etc.

Null Mixer

A null mixer consumes no controls and generates a single actuator output whose value is always zero. Typically a null mixer is used as a placeholder in a collection of mixers in order to achieve a specific pattern of actuator outputs.

The null mixer definition has the form:

Z:

Simple Mixer

A simple mixer combines zero or more control inputs into a single actuator output. Inputs are scaled, and the mixing function sums the result before applying an output scaler.

A simple mixer definition begins with:

M: <control count>
O: <-ve scale> <+ve scale> <offset> <lower limit> <upper limit>

If is zero, the sum is effectively zero and the mixer will output a fixed value that is constrained by and .

The second line defines the output scaler with scaler parameters as discussed above. Whilst the calculations are performed as floating-point operations, the values stored in the definition file are scaled by a factor of 10000; i.e. an offset of -0.5 is encoded as -5000.

The definition continues with entries describing the control inputs and their scaling, in the form:

S: <group> <index> <-ve scale> <+ve scale> <offset> <lower limit> <upper limit>

The value identifies the control group from which the scaler will read, and the value an offset within that group. These values are specific to the device reading the mixer definition.

When used to mix vehicle controls, mixer group zero is the vehicle attitude control group, and index values zero through three are normally roll, pitch, yaw and thrust respectively.

The remaining fields on the line configure the control scaler with parameters as discussed above. Whilst the calculations are performed as floating-point operations, the values stored in the definition file are scaled by a factor of 10000; i.e. an offset of -0.5 is encoded as -5000.

Multirotor Mixer

The multirotor mixer combines four control inputs (roll, pitch, yaw, thrust) into a set of actuator outputs intended to drive motor speed controllers.

The mixer definition is a single line of the form:

R: <geometry> <roll scale> <pitch scale> <yaw scale> <deadband>

The supported geometries include:

  • 4x - quadrotor in X configuration
  • 4+ - quadrotor in + configuration
  • 6x - hexcopter in X configuration
  • 6+ - hexcopter in + configuration
  • 8x - octocopter in X configuration
  • 8+ - octocopter in + configuration

Each of the roll, pitch and yaw scale values determine scaling of the roll, pitch and yaw controls relative to the thrust control. Whilst the calculations are performed as floating-point operations, the values stored in the definition file are scaled by a factor of 10000; i.e. an factor of 0.5 is encoded as 5000.

Roll, pitch and yaw inputs are expected to range from -1.0 to 1.0, whilst the thrust input ranges from 0.0 to 1.0. Output for each actuator is in the range -1.0 to 1.0.

In the case where an actuator saturates, all actuator values are rescaled so that the saturating actuator is limited to 1.0.