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Normalize all the line endings
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396 changed files with 158300 additions and 158300 deletions
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/*
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* This file is part of Cleanflight.
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*
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* Cleanflight is free software: you can redistribute it and/or modify
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* it under the terms of the GNU General Public License as published by
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* the Free Software Foundation, either version 3 of the License, or
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* (at your option) any later version.
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*
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* Cleanflight is distributed in the hope that it will be useful,
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* but WITHOUT ANY WARRANTY; without even the implied warranty of
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* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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* GNU General Public License for more details.
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*
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* You should have received a copy of the GNU General Public License
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* along with Cleanflight. If not, see <http://www.gnu.org/licenses/>.
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*/
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#pragma once
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typedef struct profile_s {
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uint8_t pidController; // 0 = multiwii original, 1 = rewrite from http://www.multiwii.com/forum/viewtopic.php?f=8&t=3671, 1, 2 = Luggi09s new baseflight pid
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pidProfile_t pidProfile;
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controlRateConfig_t controlRateConfig;
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uint8_t dynThrPID;
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uint16_t tpa_breakpoint; // Breakpoint where TPA is activated
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int16_t mag_declination; // Get your magnetic decliniation from here : http://magnetic-declination.com/
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// For example, -6deg 37min, = -637 Japan, format is [sign]dddmm (degreesminutes) default is zero.
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rollAndPitchTrims_t accelerometerTrims; // accelerometer trim
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// sensor-related stuff
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uint8_t acc_lpf_factor; // Set the Low Pass Filter factor for ACC. Increasing this value would reduce ACC noise (visible in GUI), but would increase ACC lag time. Zero = no filter
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float accz_lpf_cutoff; // cutoff frequency for the low pass filter used on the acc z-axis for althold in Hz
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accDeadband_t accDeadband;
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barometerConfig_t barometerConfig;
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uint8_t acc_unarmedcal; // turn automatic acc compensation on/off
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uint32_t activate[CHECKBOX_ITEM_COUNT]; // activate switches, bitmask, 3 bits per channel, lower 16 bits aux1-4, upper 16 bits aux 5-8
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// Radio/ESC-related configuration
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uint8_t deadband; // introduce a deadband around the stick center for pitch and roll axis. Must be greater than zero.
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uint8_t yaw_deadband; // introduce a deadband around the stick center for yaw axis. Must be greater than zero.
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uint8_t alt_hold_deadband; // defines the neutral zone of throttle stick during altitude hold, default setting is +/-40
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uint8_t alt_hold_fast_change; // when disabled, turn off the althold when throttle stick is out of deadband defined with alt_hold_deadband; when enabled, altitude changes slowly proportional to stick movement
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uint16_t throttle_correction_angle; // the angle when the throttle correction is maximal. in 0.1 degres, ex 225 = 22.5 ,30.0, 450 = 45.0 deg
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uint8_t throttle_correction_value; // the correction that will be applied at throttle_correction_angle.
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// Servo-related stuff
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servoParam_t servoConf[MAX_SUPPORTED_SERVOS]; // servo configuration
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// Failsafe related configuration
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failsafeConfig_t failsafeConfig;
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// mixer-related configuration
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mixerConfig_t mixerConfig;
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// gimbal-related configuration
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gimbalConfig_t gimbalConfig;
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#ifdef GPS
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gpsProfile_t gpsProfile;
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#endif
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} profile_t;
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/*
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* This file is part of Cleanflight.
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*
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* Cleanflight is free software: you can redistribute it and/or modify
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* it under the terms of the GNU General Public License as published by
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* the Free Software Foundation, either version 3 of the License, or
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* (at your option) any later version.
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*
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* Cleanflight is distributed in the hope that it will be useful,
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* but WITHOUT ANY WARRANTY; without even the implied warranty of
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* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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* GNU General Public License for more details.
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*
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* You should have received a copy of the GNU General Public License
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* along with Cleanflight. If not, see <http://www.gnu.org/licenses/>.
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*/
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#pragma once
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typedef struct profile_s {
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uint8_t pidController; // 0 = multiwii original, 1 = rewrite from http://www.multiwii.com/forum/viewtopic.php?f=8&t=3671, 1, 2 = Luggi09s new baseflight pid
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pidProfile_t pidProfile;
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controlRateConfig_t controlRateConfig;
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uint8_t dynThrPID;
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uint16_t tpa_breakpoint; // Breakpoint where TPA is activated
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int16_t mag_declination; // Get your magnetic decliniation from here : http://magnetic-declination.com/
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// For example, -6deg 37min, = -637 Japan, format is [sign]dddmm (degreesminutes) default is zero.
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rollAndPitchTrims_t accelerometerTrims; // accelerometer trim
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// sensor-related stuff
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uint8_t acc_lpf_factor; // Set the Low Pass Filter factor for ACC. Increasing this value would reduce ACC noise (visible in GUI), but would increase ACC lag time. Zero = no filter
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float accz_lpf_cutoff; // cutoff frequency for the low pass filter used on the acc z-axis for althold in Hz
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accDeadband_t accDeadband;
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barometerConfig_t barometerConfig;
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uint8_t acc_unarmedcal; // turn automatic acc compensation on/off
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uint32_t activate[CHECKBOX_ITEM_COUNT]; // activate switches, bitmask, 3 bits per channel, lower 16 bits aux1-4, upper 16 bits aux 5-8
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// Radio/ESC-related configuration
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uint8_t deadband; // introduce a deadband around the stick center for pitch and roll axis. Must be greater than zero.
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uint8_t yaw_deadband; // introduce a deadband around the stick center for yaw axis. Must be greater than zero.
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uint8_t alt_hold_deadband; // defines the neutral zone of throttle stick during altitude hold, default setting is +/-40
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uint8_t alt_hold_fast_change; // when disabled, turn off the althold when throttle stick is out of deadband defined with alt_hold_deadband; when enabled, altitude changes slowly proportional to stick movement
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uint16_t throttle_correction_angle; // the angle when the throttle correction is maximal. in 0.1 degres, ex 225 = 22.5 ,30.0, 450 = 45.0 deg
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uint8_t throttle_correction_value; // the correction that will be applied at throttle_correction_angle.
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// Servo-related stuff
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servoParam_t servoConf[MAX_SUPPORTED_SERVOS]; // servo configuration
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// Failsafe related configuration
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failsafeConfig_t failsafeConfig;
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// mixer-related configuration
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mixerConfig_t mixerConfig;
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// gimbal-related configuration
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gimbalConfig_t gimbalConfig;
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#ifdef GPS
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gpsProfile_t gpsProfile;
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#endif
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} profile_t;
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