/* * This file is part of Cleanflight. * * Cleanflight is free software: you can redistribute it and/or modify * it under the terms of the GNU General Public License as published by * the Free Software Foundation, either version 3 of the License, or * (at your option) any later version. * * Cleanflight is distributed in the hope that it will be useful, * but WITHOUT ANY WARRANTY; without even the implied warranty of * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the * GNU General Public License for more details. * * You should have received a copy of the GNU General Public License * along with Cleanflight. If not, see . */ #pragma once #include #include "common/time.h" #include "common/filter.h" #include "pg/pg.h" #define MAX_PID_PROCESS_DENOM 16 #define PID_CONTROLLER_BETAFLIGHT 1 #define PID_MIXER_SCALING 1000.0f #define PID_SERVO_MIXER_SCALING 0.7f #define PIDSUM_LIMIT 500 #define PIDSUM_LIMIT_YAW 400 // Scaling factors for Pids for better tunable range in configurator for betaflight pid controller. The scaling is based on legacy pid controller or previous float #define PTERM_SCALE 0.032029f #define ITERM_SCALE 0.244381f #define DTERM_SCALE 0.000529f typedef enum { PID_ROLL, PID_PITCH, PID_YAW, PID_ALT, PID_POS, PID_POSR, PID_NAVR, PID_LEVEL, PID_MAG, PID_VEL, PID_ITEM_COUNT } pidIndex_e; typedef enum { SUPEREXPO_YAW_OFF = 0, SUPEREXPO_YAW_ON, SUPEREXPO_YAW_ALWAYS } pidSuperExpoYaw_e; typedef enum { PID_STABILISATION_OFF = 0, PID_STABILISATION_ON } pidStabilisationState_e; typedef enum { PID_CRASH_RECOVERY_OFF = 0, PID_CRASH_RECOVERY_ON, PID_CRASH_RECOVERY_BEEP } pidCrashRecovery_e; typedef struct pid8_s { uint8_t P; uint8_t I; uint8_t D; } pid8_t; typedef struct pidProfile_s { pid8_t pid[PID_ITEM_COUNT]; uint16_t yaw_lowpass_hz; // Additional yaw filter when yaw axis too noisy uint16_t dterm_lowpass_hz; // Delta Filter in hz uint16_t dterm_notch_hz; // Biquad dterm notch hz uint16_t dterm_notch_cutoff; // Biquad dterm notch low cutoff uint8_t dterm_filter_type; // Filter selection for dterm uint8_t itermWindupPointPercent; // Experimental ITerm windup threshold, percent motor saturation uint16_t pidSumLimit; uint16_t pidSumLimitYaw; uint8_t vbatPidCompensation; // Scale PIDsum to battery voltage uint8_t pidAtMinThrottle; // Disable/Enable pids on zero throttle. Normally even without airmode P and D would be active. uint8_t levelAngleLimit; // Max angle in degrees in level mode uint8_t horizon_tilt_effect; // inclination factor for Horizon mode uint8_t horizon_tilt_expert_mode; // OFF or ON // Betaflight PID controller parameters uint16_t itermThrottleThreshold; // max allowed throttle delta before iterm accelerated in ms uint16_t itermAcceleratorGain; // Iterm Accelerator Gain when itermThrottlethreshold is hit uint8_t setpointRelaxRatio; // Setpoint weight relaxation effect uint8_t dtermSetpointWeight; // Setpoint weight for Dterm (0= measurement, 1= full error, 1 > aggressive derivative) uint16_t yawRateAccelLimit; // yaw accel limiter for deg/sec/ms uint16_t rateAccelLimit; // accel limiter roll/pitch deg/sec/ms uint16_t crash_dthreshold; // dterm crash value uint16_t crash_gthreshold; // gyro crash value uint16_t crash_setpoint_threshold; // setpoint must be below this value to detect crash, so flips and rolls are not interpreted as crashes uint16_t crash_time; // ms uint16_t crash_delay; // ms uint8_t crash_recovery_angle; // degrees uint8_t crash_recovery_rate; // degree/second pidCrashRecovery_e crash_recovery; // off, on, on and beeps when it is in crash recovery mode uint16_t crash_limit_yaw; // limits yaw errorRate, so crashes don't cause huge throttle increase uint16_t itermLimit; uint16_t dterm_lowpass2_hz; // Extra PT1 Filter on D in hz uint8_t throttle_boost; // how much should throttle be boosted during transient changes 0-100, 100 adds 10x hpf filtered throttle uint8_t throttle_boost_cutoff; // Which cutoff frequency to use for throttle boost. higher cutoffs keep the boost on for shorter. Specified in hz. uint8_t iterm_rotation; // rotates iterm to translate world errors to local coordinate system } pidProfile_t; #ifndef USE_OSD_SLAVE PG_DECLARE_ARRAY(pidProfile_t, MAX_PROFILE_COUNT, pidProfiles); #endif typedef struct pidConfig_s { uint8_t pid_process_denom; // Processing denominator for PID controller vs gyro sampling rate uint8_t runaway_takeoff_prevention; // off, on - enables pidsum runaway disarm logic uint16_t runaway_takeoff_deactivate_delay; // delay in ms for "in-flight" conditions before deactivation (successful flight) uint8_t runaway_takeoff_deactivate_throttle; // minimum throttle percent required during deactivation phase } pidConfig_t; PG_DECLARE(pidConfig_t, pidConfig); union rollAndPitchTrims_u; void pidController(const pidProfile_t *pidProfile, const union rollAndPitchTrims_u *angleTrim, timeUs_t currentTimeUs); extern float axisPID_P[3], axisPID_I[3], axisPID_D[3]; extern float axisPIDSum[3]; bool airmodeWasActivated; extern uint32_t targetPidLooptime; // PIDweight is a scale factor for PIDs which is derived from the throttle and TPA setting, and 100 = 100% scale means no PID reduction extern uint8_t PIDweight[3]; void pidResetITerm(void); void pidStabilisationState(pidStabilisationState_e pidControllerState); void pidSetItermAccelerator(float newItermAccelerator); void pidInitFilters(const pidProfile_t *pidProfile); void pidInitConfig(const pidProfile_t *pidProfile); void pidInit(const pidProfile_t *pidProfile); void pidCopyProfile(uint8_t dstPidProfileIndex, uint8_t srcPidProfileIndex); bool crashRecoveryModeActive(void); FAST_RAM float throttleBoost; pt1Filter_t throttleLpf;