13 changed files with 378 additions and 0 deletions
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Aileron/rudder/elevator/throttle mixer for PX4FMU |
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================================================== |
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|
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This file defines mixers suitable 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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|
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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: 1 |
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O: 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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|
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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: 1 |
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O: 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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|
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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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|
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M: 1 |
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O: 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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|
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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: 1 |
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O: 10000 10000 0 -10000 10000 |
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S: 0 3 0 20000 -10000 -10000 10000 |
@ -0,0 +1,60 @@ |
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Aileron/elevator/throttle mixer for PX4FMU |
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================================================== |
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|
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|
This file defines mixers suitable 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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|
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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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|
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Aileron mixer |
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------------- |
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Two scalers total (output, roll). |
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|
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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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|
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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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|
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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: 1 |
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O: 10000 10000 0 -10000 10000 |
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S: 0 0 10000 10000 0 -10000 10000 |
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|
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Elevator mixer |
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------------ |
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Two scalers total (output, roll). |
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|
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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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|
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M: 1 |
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O: 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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|
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Z: |
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|
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Motor speed mixer |
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----------------- |
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Two scalers total (output, thrust). |
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|
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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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|
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M: 1 |
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O: 10000 10000 0 -10000 10000 |
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S: 0 3 0 20000 -10000 -10000 10000 |
@ -0,0 +1,52 @@ |
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Delta-wing mixer for PX4FMU |
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=========================== |
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|
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Designed for Bormatec Camflyer Q |
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|
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This file defines mixers suitable for controlling a delta wing aircraft using |
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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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assumed to be unused. |
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|
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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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|
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See the README for more information on the scaler format. |
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|
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Elevon mixers |
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------------- |
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Three scalers total (output, roll, pitch). |
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|
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On the assumption that the two elevon servos are physically reversed, the pitch |
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input is inverted between the two servos. |
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|
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The scaling factor for roll inputs is adjusted to implement differential travel |
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for the elevons. |
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M: 2 |
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O: 10000 10000 0 -10000 10000 |
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S: 0 0 -5000 -8000 0 -10000 10000 |
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S: 0 1 8000 8000 0 -10000 10000 |
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M: 2 |
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O: 10000 10000 0 -10000 10000 |
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S: 0 0 -8000 -5000 0 -10000 10000 |
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S: 0 1 -8000 -8000 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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Z: |
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|
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Motor speed mixer |
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----------------- |
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Two scalers total (output, thrust). |
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|
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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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|
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M: 1 |
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O: 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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|
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This file defines mixers suitable 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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|
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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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|
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Rudder mixer |
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------------ |
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Two scalers total (output, roll). |
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|
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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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|
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M: 1 |
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O: 10000 10000 0 -10000 10000 |
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S: 0 0 10000 10000 0 -10000 10000 |
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|
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Elevator mixer |
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------------ |
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Two scalers total (output, roll). |
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|
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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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|
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M: 1 |
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O: 10000 10000 0 -10000 10000 |
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S: 0 1 -10000 -10000 0 -10000 10000 |
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|
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Output 2 |
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-------- |
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This mixer is empty. |
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|
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Z: |
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|
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Motor speed mixer |
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----------------- |
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Two scalers total (output, thrust). |
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|
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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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|
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M: 1 |
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O: 10000 10000 0 -10000 10000 |
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S: 0 3 0 20000 -10000 -10000 10000 |
@ -0,0 +1,50 @@ |
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Delta-wing mixer for PX4FMU |
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|
=========================== |
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|
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|
This file defines mixers suitable for controlling a delta wing aircraft using |
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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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assumed to be unused. |
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|
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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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|
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See the README for more information on the scaler format. |
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|
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Elevon mixers |
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|
------------- |
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Three scalers total (output, roll, pitch). |
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|
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On the assumption that the two elevon servos are physically reversed, the pitch |
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input is inverted between the two servos. |
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|
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The scaling factor for roll inputs is adjusted to implement differential travel |
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for the elevons. |
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|
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M: 2 |
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O: 10000 10000 0 -10000 10000 |
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S: 0 0 -3000 -5000 0 -10000 10000 |
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S: 0 1 -5000 -5000 0 -10000 10000 |
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M: 2 |
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O: 10000 10000 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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|
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Output 2 |
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-------- |
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This mixer is empty. |
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|
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Z: |
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|
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Motor speed mixer |
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|
----------------- |
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Two scalers total (output, thrust). |
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|
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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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|
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M: 1 |
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O: 10000 10000 0 -10000 10000 |
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S: 0 3 0 20000 -10000 -10000 10000 |
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@ -0,0 +1,50 @@ |
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Delta-wing mixer for PX4FMU |
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|
=========================== |
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|
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|
This file defines mixers suitable for controlling a delta wing aircraft using |
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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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|
assumed to be unused. |
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|
|
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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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|
|
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See the README for more information on the scaler format. |
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|
|
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|
Elevon mixers |
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|
------------- |
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|
Three scalers total (output, roll, pitch). |
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|
|
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|
On the assumption that the two elevon servos are physically reversed, the pitch |
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|
input is inverted between the two servos. |
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|
|
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|
The scaling factor for roll inputs is adjusted to implement differential travel |
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|
for the elevons. |
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|
|
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M: 2 |
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O: 10000 10000 0 -10000 10000 |
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S: 0 0 3000 5000 0 -10000 10000 |
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S: 0 1 5000 5000 0 -10000 10000 |
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|
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M: 2 |
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O: 10000 10000 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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|
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Output 2 |
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-------- |
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This mixer is empty. |
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|
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Z: |
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|
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Motor speed mixer |
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|
----------------- |
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Two scalers total (output, thrust). |
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|
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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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|
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M: 1 |
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O: 10000 10000 0 -10000 10000 |
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S: 0 3 0 20000 -10000 -10000 10000 |
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@ -0,0 +1,7 @@ |
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Multirotor mixer for PX4FMU |
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=========================== |
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|
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This file defines a single mixer for a hexacopter in the + configuration. All controls |
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are mixed 100%. |
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|
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R: 6+ 10000 10000 10000 0 |
@ -0,0 +1,7 @@ |
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Multirotor mixer for PX4FMU |
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=========================== |
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|
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This file defines a single mixer for a hexacopter in the X configuration. All controls |
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are mixed 100%. |
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|
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R: 6x 10000 10000 10000 0 |
@ -0,0 +1,7 @@ |
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Multirotor mixer for PX4FMU |
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=========================== |
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|
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This file defines a single mixer for a octocopter in the + configuration. All controls |
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are mixed 100%. |
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|
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R: 8+ 10000 10000 10000 0 |
@ -0,0 +1,7 @@ |
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Multirotor mixer for PX4FMU |
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=========================== |
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|
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This file defines a single mixer for a octocopter in the X configuration. All controls |
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are mixed 100%. |
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|
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R: 8x 10000 10000 10000 0 |
@ -0,0 +1,7 @@ |
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Multirotor mixer for PX4FMU |
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=========================== |
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|
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This file defines a single mixer for a quadrotor in the + configuration. All controls |
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are mixed 100%. |
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|
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R: 4+ 10000 10000 10000 0 |
@ -0,0 +1,7 @@ |
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|
Multirotor mixer for PX4FMU |
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|
=========================== |
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|
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This file defines a single mixer for a quadrotor in the V configuration. All controls |
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|
are mixed 100%. |
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|
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R: 4v 10000 10000 10000 0 |
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Reference in new issue