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Lorenz Meier b42c1123a2 ROMFS: Add flaps and gear mixers to all standard planes 8 years ago
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AAERTWF.main.mix
AAVVTWFF.main.mix
AERT.main.mix ROMFS: Add flaps and gear mixers to all standard planes 8 years ago
AET.main.mix ROMFS: Add flaps and gear mixers to all standard planes 8 years ago
AETR.main.mix ROMFS: Add flaps and gear mixers to all standard planes 8 years ago
CCPM.main.mix
FMU_pass.mix
FX79.main.mix
IO_pass.main.mix
IO_pass.mix
Q.main.mix
README.md
RET.main.mix
Viper.main.mix
X5.main.mix
bebop.main.mix Mixers: Disable on unreachable boards 8 years ago
blade130.main.mix Generic helicopter mixer 8 years ago
caipi.main.mix mixer: Removed the pitch offset in the mixer file for the TBS Caipirinha since it should be handled by either hardware installation or trim parameter 8 years ago
caipirinha_vtol.main.mix
claire.aux.mix Update claire.aux.mix 8 years ago
claire.main.mix Quad tilt vtol config (#4473) 9 years ago
coax.main.mix Removed 'degree' character that caused python3 to act up while pruning the mixer file 8 years ago
delta.main.mix
dodeca_bottom_cox.aux.mix Dodeca mixer using the AUX channels (#7532) 8 years ago
dodeca_top_cox.main.mix Dodeca mixer using the AUX channels (#7532) 8 years ago
easystar.main.mix
firefly6.aux.mix
firefly6.main.mix
hexa_+.main.mix
hexa_cox.main.mix
hexa_x.main.mix posix-configs: use 'mixer append' command for typhoon mount mixer 9 years ago
mount.aux.mix mount.aux.mix: remove the mode channel 8 years ago
mount_legs.aux.mix tap: add landing gear capability 8 years ago
ocpoc_quad_x.main.mix mixers: add default mixer for Aerotenna OcPoC-Zynq hardware 8 years ago
octo_+.main.mix
octo_cox.main.mix
octo_cox_w.main.mix
octo_x.main.mix
pass.aux.mix
phantom.main.mix
quad_+.main.mix Quad mixers: Add AUX1-2 passthrough 9 years ago
quad_+_vtol.main.mix
quad_dc.main.mix Fix usage of Iris mixer, make space by deleting unused files 8 years ago
quad_h.main.mix Quad mixers: Add AUX1-2 passthrough 9 years ago
quad_s250aq.main.mix add new asymmetric airframe for Spedix S250AQ 8 years ago
quad_w.main.mix Quad mixers: Add AUX1-2 passthrough 9 years ago
quad_x.main.mix Quad mixers: Add AUX1-2 passthrough 9 years ago
quad_x_can.main.mix Performance audit (intentionally duplicates #6829) (#6847) 8 years ago
quad_x_vtol.main.mix Get closer to correct tailsitter mixer, still incomplete 9 years ago
skywalker.main.mix
stampede.main.mix unmanned ground vehicle (UGV) controllers and Traxxas Stampede configuration (#7175) 8 years ago
tri_y_yaw+.main.mix
tri_y_yaw-.main.mix
vtol_AAERT.aux.mix
vtol_AAVVT.aux.mix
vtol_convergence.main.mix Convergence: increase yaw output in mixer 8 years ago
vtol_delta.aux.mix vtol delta quad plane: adjusted mixer scaling 9 years ago
vtol_quad_x.main.mix
wingwing.main.mix
zmr250.main.mix Mixers: Disable on unreachable boards 8 years ago

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.