From 83652794c7709ee8058587a99e81826d4959ed49 Mon Sep 17 00:00:00 2001 From: Simon Wilks Date: Tue, 15 Jul 2014 00:06:24 +0200 Subject: [PATCH 1/3] Add a mixer for the Phantom so it can be uniquely adjusted for this airframe. --- ROMFS/px4fmu_common/init.d/3031_phantom | 2 +- ROMFS/px4fmu_common/mixers/phantom.mix | 69 +++++++++++++++++++++++++ 2 files changed, 70 insertions(+), 1 deletion(-) create mode 100644 ROMFS/px4fmu_common/mixers/phantom.mix diff --git a/ROMFS/px4fmu_common/init.d/3031_phantom b/ROMFS/px4fmu_common/init.d/3031_phantom index d05c3174f9..654b0bdab1 100644 --- a/ROMFS/px4fmu_common/init.d/3031_phantom +++ b/ROMFS/px4fmu_common/init.d/3031_phantom @@ -36,7 +36,7 @@ then param set FW_T_TIME_CONST 5 fi -set MIXER FMU_Q +set MIXER phantom # Provide ESC a constant 1000 us pulse set PWM_OUTPUTS 4 diff --git a/ROMFS/px4fmu_common/mixers/phantom.mix b/ROMFS/px4fmu_common/mixers/phantom.mix new file mode 100644 index 0000000000..7fe6dc0551 --- /dev/null +++ b/ROMFS/px4fmu_common/mixers/phantom.mix @@ -0,0 +1,69 @@ +Delta-wing mixer for PX4FMU +=========================== + +Designed for the Phantom FX-61 + +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 +O: 10000 10000 0 -10000 10000 +S: 0 0 -6000 -6000 0 -10000 10000 +S: 0 1 6500 6500 0 -10000 10000 + +M: 2 +O: 10000 10000 0 -10000 10000 +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 +O: 10000 10000 0 -10000 10000 +S: 0 3 0 20000 -10000 -10000 10000 + +Gimbal / flaps / payload mixer for last four channels +----------------------------------------------------- + +M: 1 +O: 10000 10000 0 -10000 10000 +S: 0 4 10000 10000 0 -10000 10000 + +M: 1 +O: 10000 10000 0 -10000 10000 +S: 0 5 10000 10000 0 -10000 10000 + +M: 1 +O: 10000 10000 0 -10000 10000 +S: 0 6 10000 10000 0 -10000 10000 + +M: 1 +O: 10000 10000 0 -10000 10000 +S: 0 7 10000 10000 0 -10000 10000 From 9f837267de861cfd8313984f2ec64b8482a72161 Mon Sep 17 00:00:00 2001 From: Simon Wilks Date: Tue, 15 Jul 2014 00:10:08 +0200 Subject: [PATCH 2/3] Updated the comments. --- ROMFS/px4fmu_common/mixers/phantom.mix | 6 ++---- 1 file changed, 2 insertions(+), 4 deletions(-) diff --git a/ROMFS/px4fmu_common/mixers/phantom.mix b/ROMFS/px4fmu_common/mixers/phantom.mix index 7fe6dc0551..00c37a16c1 100644 --- a/ROMFS/px4fmu_common/mixers/phantom.mix +++ b/ROMFS/px4fmu_common/mixers/phantom.mix @@ -1,7 +1,5 @@ -Delta-wing mixer for PX4FMU -=========================== - -Designed for the Phantom FX-61 +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 From e91a4217ad23a0f5190b0e34b7621a5170632a43 Mon Sep 17 00:00:00 2001 From: Lorenz Meier Date: Tue, 15 Jul 2014 07:54:12 +0200 Subject: [PATCH 3/3] Fix warning --- src/modules/commander/airspeed_calibration.cpp | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/src/modules/commander/airspeed_calibration.cpp b/src/modules/commander/airspeed_calibration.cpp index 598cfe9e2d..0e58c68b60 100644 --- a/src/modules/commander/airspeed_calibration.cpp +++ b/src/modules/commander/airspeed_calibration.cpp @@ -186,7 +186,7 @@ int do_airspeed_calibration(int mavlink_fd) usleep(500 * 1000); calibration_counter = 0; - const int maxcount = 3000; + const unsigned maxcount = 3000; /* just take a few samples and make sure pitot tubes are not reversed, timeout after ~30 seconds */ while (calibration_counter < maxcount) {