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airframes: add new airframe for ThunderFly TF-G2 autogyro (#16551)
Co-authored-by: Roman Dvorak <romandvorak@mlab.cz>
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49
ROMFS/px4fmu_common/init.d/airframes/17003_TF-G2
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49
ROMFS/px4fmu_common/init.d/airframes/17003_TF-G2
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#!/bin/sh
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#
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# @name ThunderFly TF-G2
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#
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# @type Autogyro
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# @class Autogyro
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#
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# @output MAIN2 rotor_head_L
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# @output MAIN3 rotor_head_R
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# @output MAIN4 rudder
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# @output MAIN5 throttle
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#
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#
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# @url https://github.com/ThunderFly-aerospace/TF-G2/
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# @maintainer ThunderFly s.r.o., Roman Dvorak <dvorakroman@thunderfly.cz>
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#
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# @board px4_fmu-v2 exclude
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# @board intel_aerofc-v1 exclude
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# @board bitcraze_crazyflie exclude
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#
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. ${R}etc/init.d/rc.fw_defaults
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if [ $AUTOCNF = yes ]
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then
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param set BAT_CAPACITY 3300
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param set BAT_N_CELLS 3
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param set PWM_AUX_RATE 50
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param set PWM_RATE 50
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param set SENS_BOARD_ROT 4
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param set FW_AIRSPD_MAX 20
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param set FW_AIRSPD_MIN 7
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param set FW_AIRSPD_TRIM 13
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param set FW_THR_CRUISE 0.8
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param set FW_MAN_P_MAX 25
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param set FW_MAN_R_MAX 25
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param set FW_PR_I 0.02
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param set FW_R_LIM 40
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param set FW_P_LIM_MAX 25
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param set FW_P_LIM_MIN -5
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param set FW_P_RMAX_NEG 20
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fi
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set MIXER TF-G2
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set MIXER_AUX pass
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@ -146,7 +146,9 @@ px4_add_romfs_files(
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16001_helicopter
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# [17000, 17999] Autogyro
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17002_TF-AutoG2
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17003_TF-G2
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24001_dodeca_cox
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39
ROMFS/px4fmu_common/mixers/TF-G2.main.mix
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ROMFS/px4fmu_common/mixers/TF-G2.main.mix
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TF-G2 autogyro mixer
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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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CH1: empty - fixing cuav nano jittering of 1st output.
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Z:
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CH2, 3: rotor-head mixer
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-------------
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Two scalers total (output, roll).
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M: 2
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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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S: 0 1 10000 10000 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 -10000 -10000 0 -10000 10000
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S: 0 1 -10000 -10000 0 -10000 10000
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CH4: Rudder mixer
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------------
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Two scalers total (output, yaw).
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M: 1
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S: 0 2 10000 10000 0 -10000 10000
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CH5: Motor speed mixer
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-----------------
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Two scalers total (output, thrust).
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M: 1
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S: 0 3 0 20000 -10000 -10000 10000
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