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betaflight/src/main/blackbox/blackbox.c
Bruce Luckcuck 9315b8f1b6 Fix RTC local time formatting (timezone offset) when no valid date/time 
Timezone shouldn't be applied to the "default" invalid date as it can cause underflow for negative timezone offsets.
2019-08-17 11:30:07 -04:00

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/*
* This file is part of Cleanflight and Betaflight.
*
* Cleanflight and Betaflight are free software. You can redistribute
* this software and/or modify this software 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 and Betaflight are distributed in the hope that they
* 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 this software.
*
* If not, see <http://www.gnu.org/licenses/>.
*/
#include <stdbool.h>
#include <stdint.h>
#include <string.h>
#include <math.h>
#include "platform.h"
#ifdef USE_BLACKBOX
#include "blackbox.h"
#include "blackbox_encoding.h"
#include "blackbox_fielddefs.h"
#include "blackbox_io.h"
#include "build/build_config.h"
#include "build/debug.h"
#include "build/version.h"
#include "common/axis.h"
#include "common/encoding.h"
#include "common/maths.h"
#include "common/time.h"
#include "common/utils.h"
#include "config/feature.h"
#include "pg/pg.h"
#include "pg/pg_ids.h"
#include "pg/motor.h"
#include "pg/rx.h"
#include "drivers/compass/compass.h"
#include "drivers/sensor.h"
#include "drivers/time.h"
#include "fc/config.h"
#include "fc/controlrate_profile.h"
#include "fc/rc.h"
#include "fc/rc_controls.h"
#include "fc/rc_modes.h"
#include "fc/runtime_config.h"
#include "flight/failsafe.h"
#include "flight/mixer.h"
#include "flight/pid.h"
#include "flight/servos.h"
#include "io/beeper.h"
#include "io/gps.h"
#include "io/serial.h"
#include "rx/rx.h"
#include "sensors/acceleration.h"
#include "sensors/barometer.h"
#include "sensors/battery.h"
#include "sensors/compass.h"
#include "sensors/gyro.h"
#include "sensors/rangefinder.h"
#if defined(ENABLE_BLACKBOX_LOGGING_ON_SPIFLASH_BY_DEFAULT)
#define DEFAULT_BLACKBOX_DEVICE BLACKBOX_DEVICE_FLASH
#elif defined(ENABLE_BLACKBOX_LOGGING_ON_SDCARD_BY_DEFAULT)
#define DEFAULT_BLACKBOX_DEVICE BLACKBOX_DEVICE_SDCARD
#else
#define DEFAULT_BLACKBOX_DEVICE BLACKBOX_DEVICE_SERIAL
#endif
PG_REGISTER_WITH_RESET_TEMPLATE(blackboxConfig_t, blackboxConfig, PG_BLACKBOX_CONFIG, 1);
PG_RESET_TEMPLATE(blackboxConfig_t, blackboxConfig,
.p_ratio = 32,
.device = DEFAULT_BLACKBOX_DEVICE,
.record_acc = 1,
.mode = BLACKBOX_MODE_NORMAL
);
#define BLACKBOX_SHUTDOWN_TIMEOUT_MILLIS 200
// Some macros to make writing FLIGHT_LOG_FIELD_* constants shorter:
#define PREDICT(x) CONCAT(FLIGHT_LOG_FIELD_PREDICTOR_, x)
#define ENCODING(x) CONCAT(FLIGHT_LOG_FIELD_ENCODING_, x)
#define CONDITION(x) CONCAT(FLIGHT_LOG_FIELD_CONDITION_, x)
#define UNSIGNED FLIGHT_LOG_FIELD_UNSIGNED
#define SIGNED FLIGHT_LOG_FIELD_SIGNED
static const char blackboxHeader[] =
"H Product:Blackbox flight data recorder by Nicholas Sherlock\n"
"H Data version:2\n";
static const char* const blackboxFieldHeaderNames[] = {
"name",
"signed",
"predictor",
"encoding",
"predictor",
"encoding"
};
/* All field definition structs should look like this (but with longer arrs): */
typedef struct blackboxFieldDefinition_s {
const char *name;
// If the field name has a number to be included in square brackets [1] afterwards, set it here, or -1 for no brackets:
int8_t fieldNameIndex;
// Each member of this array will be the value to print for this field for the given header index
uint8_t arr[1];
} blackboxFieldDefinition_t;
#define BLACKBOX_DELTA_FIELD_HEADER_COUNT ARRAYLEN(blackboxFieldHeaderNames)
#define BLACKBOX_SIMPLE_FIELD_HEADER_COUNT (BLACKBOX_DELTA_FIELD_HEADER_COUNT - 2)
#define BLACKBOX_CONDITIONAL_FIELD_HEADER_COUNT (BLACKBOX_DELTA_FIELD_HEADER_COUNT - 2)
typedef struct blackboxSimpleFieldDefinition_s {
const char *name;
int8_t fieldNameIndex;
uint8_t isSigned;
uint8_t predict;
uint8_t encode;
} blackboxSimpleFieldDefinition_t;
typedef struct blackboxConditionalFieldDefinition_s {
const char *name;
int8_t fieldNameIndex;
uint8_t isSigned;
uint8_t predict;
uint8_t encode;
uint8_t condition; // Decide whether this field should appear in the log
} blackboxConditionalFieldDefinition_t;
typedef struct blackboxDeltaFieldDefinition_s {
const char *name;
int8_t fieldNameIndex;
uint8_t isSigned;
uint8_t Ipredict;
uint8_t Iencode;
uint8_t Ppredict;
uint8_t Pencode;
uint8_t condition; // Decide whether this field should appear in the log
} blackboxDeltaFieldDefinition_t;
/**
* Description of the blackbox fields we are writing in our main intra (I) and inter (P) frames. This description is
* written into the flight log header so the log can be properly interpreted (but these definitions don't actually cause
* the encoding to happen, we have to encode the flight log ourselves in write{Inter|Intra}frame() in a way that matches
* the encoding we've promised here).
*/
static const blackboxDeltaFieldDefinition_t blackboxMainFields[] = {
/* loopIteration doesn't appear in P frames since it always increments */
{"loopIteration",-1, UNSIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(UNSIGNED_VB), .Ppredict = PREDICT(INC), .Pencode = FLIGHT_LOG_FIELD_ENCODING_NULL, CONDITION(ALWAYS)},
/* Time advances pretty steadily so the P-frame prediction is a straight line */
{"time", -1, UNSIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(UNSIGNED_VB), .Ppredict = PREDICT(STRAIGHT_LINE), .Pencode = ENCODING(SIGNED_VB), CONDITION(ALWAYS)},
{"axisP", 0, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(SIGNED_VB), CONDITION(ALWAYS)},
{"axisP", 1, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(SIGNED_VB), CONDITION(ALWAYS)},
{"axisP", 2, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(SIGNED_VB), CONDITION(ALWAYS)},
/* I terms get special packed encoding in P frames: */
{"axisI", 0, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(TAG2_3S32), CONDITION(ALWAYS)},
{"axisI", 1, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(TAG2_3S32), CONDITION(ALWAYS)},
{"axisI", 2, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(TAG2_3S32), CONDITION(ALWAYS)},
{"axisD", 0, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(SIGNED_VB), CONDITION(NONZERO_PID_D_0)},
{"axisD", 1, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(SIGNED_VB), CONDITION(NONZERO_PID_D_1)},
{"axisD", 2, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(SIGNED_VB), CONDITION(NONZERO_PID_D_2)},
{"axisF", 0, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(SIGNED_VB), CONDITION(ALWAYS)},
{"axisF", 1, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(SIGNED_VB), CONDITION(ALWAYS)},
{"axisF", 2, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(SIGNED_VB), CONDITION(ALWAYS)},
/* rcCommands are encoded together as a group in P-frames: */
{"rcCommand", 0, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(TAG8_4S16), CONDITION(ALWAYS)},
{"rcCommand", 1, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(TAG8_4S16), CONDITION(ALWAYS)},
{"rcCommand", 2, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(TAG8_4S16), CONDITION(ALWAYS)},
{"rcCommand", 3, UNSIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(UNSIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(TAG8_4S16), CONDITION(ALWAYS)},
// setpoint - define 4 fields like rcCommand to use the same encoding. setpoint[4] contains the mixer throttle
{"setpoint", 0, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(TAG8_4S16), CONDITION(ALWAYS)},
{"setpoint", 1, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(TAG8_4S16), CONDITION(ALWAYS)},
{"setpoint", 2, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(TAG8_4S16), CONDITION(ALWAYS)},
{"setpoint", 3, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(TAG8_4S16), CONDITION(ALWAYS)},
{"vbatLatest", -1, UNSIGNED, .Ipredict = PREDICT(VBATREF), .Iencode = ENCODING(NEG_14BIT), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(TAG8_8SVB), FLIGHT_LOG_FIELD_CONDITION_VBAT},
{"amperageLatest",-1, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(TAG8_8SVB), FLIGHT_LOG_FIELD_CONDITION_AMPERAGE_ADC},
#ifdef USE_MAG
{"magADC", 0, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(TAG8_8SVB), FLIGHT_LOG_FIELD_CONDITION_MAG},
{"magADC", 1, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(TAG8_8SVB), FLIGHT_LOG_FIELD_CONDITION_MAG},
{"magADC", 2, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(TAG8_8SVB), FLIGHT_LOG_FIELD_CONDITION_MAG},
#endif
#ifdef USE_BARO
{"BaroAlt", -1, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(TAG8_8SVB), FLIGHT_LOG_FIELD_CONDITION_BARO},
#endif
#ifdef USE_RANGEFINDER
{"surfaceRaw", -1, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(TAG8_8SVB), FLIGHT_LOG_FIELD_CONDITION_RANGEFINDER},
#endif
{"rssi", -1, UNSIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(UNSIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(TAG8_8SVB), FLIGHT_LOG_FIELD_CONDITION_RSSI},
/* Gyros and accelerometers base their P-predictions on the average of the previous 2 frames to reduce noise impact */
{"gyroADC", 0, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(AVERAGE_2), .Pencode = ENCODING(SIGNED_VB), CONDITION(ALWAYS)},
{"gyroADC", 1, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(AVERAGE_2), .Pencode = ENCODING(SIGNED_VB), CONDITION(ALWAYS)},
{"gyroADC", 2, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(AVERAGE_2), .Pencode = ENCODING(SIGNED_VB), CONDITION(ALWAYS)},
{"accSmooth", 0, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(AVERAGE_2), .Pencode = ENCODING(SIGNED_VB), FLIGHT_LOG_FIELD_CONDITION_ACC},
{"accSmooth", 1, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(AVERAGE_2), .Pencode = ENCODING(SIGNED_VB), FLIGHT_LOG_FIELD_CONDITION_ACC},
{"accSmooth", 2, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(AVERAGE_2), .Pencode = ENCODING(SIGNED_VB), FLIGHT_LOG_FIELD_CONDITION_ACC},
{"debug", 0, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(AVERAGE_2), .Pencode = ENCODING(SIGNED_VB), FLIGHT_LOG_FIELD_CONDITION_DEBUG},
{"debug", 1, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(AVERAGE_2), .Pencode = ENCODING(SIGNED_VB), FLIGHT_LOG_FIELD_CONDITION_DEBUG},
{"debug", 2, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(AVERAGE_2), .Pencode = ENCODING(SIGNED_VB), FLIGHT_LOG_FIELD_CONDITION_DEBUG},
{"debug", 3, SIGNED, .Ipredict = PREDICT(0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(AVERAGE_2), .Pencode = ENCODING(SIGNED_VB), FLIGHT_LOG_FIELD_CONDITION_DEBUG},
/* Motors only rarely drops under minthrottle (when stick falls below mincommand), so predict minthrottle for it and use *unsigned* encoding (which is large for negative numbers but more compact for positive ones): */
{"motor", 0, UNSIGNED, .Ipredict = PREDICT(MINMOTOR), .Iencode = ENCODING(UNSIGNED_VB), .Ppredict = PREDICT(AVERAGE_2), .Pencode = ENCODING(SIGNED_VB), CONDITION(AT_LEAST_MOTORS_1)},
/* Subsequent motors base their I-frame values on the first one, P-frame values on the average of last two frames: */
{"motor", 1, UNSIGNED, .Ipredict = PREDICT(MOTOR_0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(AVERAGE_2), .Pencode = ENCODING(SIGNED_VB), CONDITION(AT_LEAST_MOTORS_2)},
{"motor", 2, UNSIGNED, .Ipredict = PREDICT(MOTOR_0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(AVERAGE_2), .Pencode = ENCODING(SIGNED_VB), CONDITION(AT_LEAST_MOTORS_3)},
{"motor", 3, UNSIGNED, .Ipredict = PREDICT(MOTOR_0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(AVERAGE_2), .Pencode = ENCODING(SIGNED_VB), CONDITION(AT_LEAST_MOTORS_4)},
{"motor", 4, UNSIGNED, .Ipredict = PREDICT(MOTOR_0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(AVERAGE_2), .Pencode = ENCODING(SIGNED_VB), CONDITION(AT_LEAST_MOTORS_5)},
{"motor", 5, UNSIGNED, .Ipredict = PREDICT(MOTOR_0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(AVERAGE_2), .Pencode = ENCODING(SIGNED_VB), CONDITION(AT_LEAST_MOTORS_6)},
{"motor", 6, UNSIGNED, .Ipredict = PREDICT(MOTOR_0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(AVERAGE_2), .Pencode = ENCODING(SIGNED_VB), CONDITION(AT_LEAST_MOTORS_7)},
{"motor", 7, UNSIGNED, .Ipredict = PREDICT(MOTOR_0), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(AVERAGE_2), .Pencode = ENCODING(SIGNED_VB), CONDITION(AT_LEAST_MOTORS_8)},
/* Tricopter tail servo */
{"servo", 5, UNSIGNED, .Ipredict = PREDICT(1500), .Iencode = ENCODING(SIGNED_VB), .Ppredict = PREDICT(PREVIOUS), .Pencode = ENCODING(SIGNED_VB), CONDITION(TRICOPTER)}
};
#ifdef USE_GPS
// GPS position/vel frame
static const blackboxConditionalFieldDefinition_t blackboxGpsGFields[] = {
{"time", -1, UNSIGNED, PREDICT(LAST_MAIN_FRAME_TIME), ENCODING(UNSIGNED_VB), CONDITION(NOT_LOGGING_EVERY_FRAME)},
{"GPS_numSat", -1, UNSIGNED, PREDICT(0), ENCODING(UNSIGNED_VB), CONDITION(ALWAYS)},
{"GPS_coord", 0, SIGNED, PREDICT(HOME_COORD), ENCODING(SIGNED_VB), CONDITION(ALWAYS)},
{"GPS_coord", 1, SIGNED, PREDICT(HOME_COORD), ENCODING(SIGNED_VB), CONDITION(ALWAYS)},
{"GPS_altitude", -1, UNSIGNED, PREDICT(0), ENCODING(UNSIGNED_VB), CONDITION(ALWAYS)},
{"GPS_speed", -1, UNSIGNED, PREDICT(0), ENCODING(UNSIGNED_VB), CONDITION(ALWAYS)},
{"GPS_ground_course", -1, UNSIGNED, PREDICT(0), ENCODING(UNSIGNED_VB), CONDITION(ALWAYS)}
};
// GPS home frame
static const blackboxSimpleFieldDefinition_t blackboxGpsHFields[] = {
{"GPS_home", 0, SIGNED, PREDICT(0), ENCODING(SIGNED_VB)},
{"GPS_home", 1, SIGNED, PREDICT(0), ENCODING(SIGNED_VB)}
};
#endif
// Rarely-updated fields
static const blackboxSimpleFieldDefinition_t blackboxSlowFields[] = {
{"flightModeFlags", -1, UNSIGNED, PREDICT(0), ENCODING(UNSIGNED_VB)},
{"stateFlags", -1, UNSIGNED, PREDICT(0), ENCODING(UNSIGNED_VB)},
{"failsafePhase", -1, UNSIGNED, PREDICT(0), ENCODING(TAG2_3S32)},
{"rxSignalReceived", -1, UNSIGNED, PREDICT(0), ENCODING(TAG2_3S32)},
{"rxFlightChannelsValid", -1, UNSIGNED, PREDICT(0), ENCODING(TAG2_3S32)}
};
typedef enum BlackboxState {
BLACKBOX_STATE_DISABLED = 0,
BLACKBOX_STATE_STOPPED,
BLACKBOX_STATE_PREPARE_LOG_FILE,
BLACKBOX_STATE_SEND_HEADER,
BLACKBOX_STATE_SEND_MAIN_FIELD_HEADER,
BLACKBOX_STATE_SEND_GPS_H_HEADER,
BLACKBOX_STATE_SEND_GPS_G_HEADER,
BLACKBOX_STATE_SEND_SLOW_HEADER,
BLACKBOX_STATE_SEND_SYSINFO,
BLACKBOX_STATE_PAUSED,
BLACKBOX_STATE_RUNNING,
BLACKBOX_STATE_SHUTTING_DOWN,
BLACKBOX_STATE_START_ERASE,
BLACKBOX_STATE_ERASING,
BLACKBOX_STATE_ERASED
} BlackboxState;
typedef struct blackboxMainState_s {
uint32_t time;
int32_t axisPID_P[XYZ_AXIS_COUNT];
int32_t axisPID_I[XYZ_AXIS_COUNT];
int32_t axisPID_D[XYZ_AXIS_COUNT];
int32_t axisPID_F[XYZ_AXIS_COUNT];
int16_t rcCommand[4];
int16_t setpoint[4];
int16_t gyroADC[XYZ_AXIS_COUNT];
int16_t accADC[XYZ_AXIS_COUNT];
int16_t debug[DEBUG16_VALUE_COUNT];
int16_t motor[MAX_SUPPORTED_MOTORS];
int16_t servo[MAX_SUPPORTED_SERVOS];
uint16_t vbatLatest;
int32_t amperageLatest;
#ifdef USE_BARO
int32_t BaroAlt;
#endif
#ifdef USE_MAG
int16_t magADC[XYZ_AXIS_COUNT];
#endif
#ifdef USE_RANGEFINDER
int32_t surfaceRaw;
#endif
uint16_t rssi;
} blackboxMainState_t;
typedef struct blackboxGpsState_s {
int32_t GPS_home[2];
int32_t GPS_coord[2];
uint8_t GPS_numSat;
} blackboxGpsState_t;
// This data is updated really infrequently:
typedef struct blackboxSlowState_s {
uint32_t flightModeFlags; // extend this data size (from uint16_t)
uint8_t stateFlags;
uint8_t failsafePhase;
bool rxSignalReceived;
bool rxFlightChannelsValid;
} __attribute__((__packed__)) blackboxSlowState_t; // We pack this struct so that padding doesn't interfere with memcmp()
//From rc_controls.c
extern boxBitmask_t rcModeActivationMask;
static BlackboxState blackboxState = BLACKBOX_STATE_DISABLED;
static uint32_t blackboxLastArmingBeep = 0;
static uint32_t blackboxLastFlightModeFlags = 0; // New event tracking of flight modes
static struct {
uint32_t headerIndex;
/* Since these fields are used during different blackbox states (never simultaneously) we can
* overlap them to save on RAM
*/
union {
int fieldIndex;
uint32_t startTime;
} u;
} xmitState;
// Cache for FLIGHT_LOG_FIELD_CONDITION_* test results:
static uint32_t blackboxConditionCache;
STATIC_ASSERT((sizeof(blackboxConditionCache) * 8) >= FLIGHT_LOG_FIELD_CONDITION_LAST, too_many_flight_log_conditions);
static uint32_t blackboxIteration;
static uint16_t blackboxLoopIndex;
static uint16_t blackboxPFrameIndex;
static uint16_t blackboxIFrameIndex;
// number of flight loop iterations before logging I-frame
// typically 32 for 1kHz loop, 64 for 2kHz loop etc
STATIC_UNIT_TESTED int16_t blackboxIInterval = 0;
// number of flight loop iterations before logging P-frame
STATIC_UNIT_TESTED int16_t blackboxPInterval = 0;
STATIC_UNIT_TESTED int32_t blackboxSInterval = 0;
STATIC_UNIT_TESTED int32_t blackboxSlowFrameIterationTimer;
static bool blackboxLoggedAnyFrames;
/*
* We store voltages in I-frames relative to this, which was the voltage when the blackbox was activated.
* This helps out since the voltage is only expected to fall from that point and we can reduce our diffs
* to encode:
*/
static uint16_t vbatReference;
static blackboxGpsState_t gpsHistory;
static blackboxSlowState_t slowHistory;
// Keep a history of length 2, plus a buffer for MW to store the new values into
static blackboxMainState_t blackboxHistoryRing[3];
// These point into blackboxHistoryRing, use them to know where to store history of a given age (0, 1 or 2 generations old)
static blackboxMainState_t* blackboxHistory[3];
static bool blackboxModeActivationConditionPresent = false;
/**
* Return true if it is safe to edit the Blackbox configuration.
*/
bool blackboxMayEditConfig(void)
{
return blackboxState <= BLACKBOX_STATE_STOPPED;
}
static bool blackboxIsOnlyLoggingIntraframes(void)
{
return blackboxConfig()->p_ratio == 0;
}
static bool testBlackboxConditionUncached(FlightLogFieldCondition condition)
{
switch (condition) {
case FLIGHT_LOG_FIELD_CONDITION_ALWAYS:
return true;
case FLIGHT_LOG_FIELD_CONDITION_AT_LEAST_MOTORS_1:
case FLIGHT_LOG_FIELD_CONDITION_AT_LEAST_MOTORS_2:
case FLIGHT_LOG_FIELD_CONDITION_AT_LEAST_MOTORS_3:
case FLIGHT_LOG_FIELD_CONDITION_AT_LEAST_MOTORS_4:
case FLIGHT_LOG_FIELD_CONDITION_AT_LEAST_MOTORS_5:
case FLIGHT_LOG_FIELD_CONDITION_AT_LEAST_MOTORS_6:
case FLIGHT_LOG_FIELD_CONDITION_AT_LEAST_MOTORS_7:
case FLIGHT_LOG_FIELD_CONDITION_AT_LEAST_MOTORS_8:
return getMotorCount() >= condition - FLIGHT_LOG_FIELD_CONDITION_AT_LEAST_MOTORS_1 + 1;
case FLIGHT_LOG_FIELD_CONDITION_TRICOPTER:
return mixerConfig()->mixerMode == MIXER_TRI || mixerConfig()->mixerMode == MIXER_CUSTOM_TRI;
case FLIGHT_LOG_FIELD_CONDITION_NONZERO_PID_D_0:
case FLIGHT_LOG_FIELD_CONDITION_NONZERO_PID_D_1:
case FLIGHT_LOG_FIELD_CONDITION_NONZERO_PID_D_2:
return currentPidProfile->pid[condition - FLIGHT_LOG_FIELD_CONDITION_NONZERO_PID_D_0].D != 0;
case FLIGHT_LOG_FIELD_CONDITION_MAG:
#ifdef USE_MAG
return sensors(SENSOR_MAG);
#else
return false;
#endif
case FLIGHT_LOG_FIELD_CONDITION_BARO:
#ifdef USE_BARO
return sensors(SENSOR_BARO);
#else
return false;
#endif
case FLIGHT_LOG_FIELD_CONDITION_VBAT:
return batteryConfig()->voltageMeterSource != VOLTAGE_METER_NONE;
case FLIGHT_LOG_FIELD_CONDITION_AMPERAGE_ADC:
return (batteryConfig()->currentMeterSource != CURRENT_METER_NONE) && (batteryConfig()->currentMeterSource != CURRENT_METER_VIRTUAL);
case FLIGHT_LOG_FIELD_CONDITION_RANGEFINDER:
#ifdef USE_RANGEFINDER
return sensors(SENSOR_RANGEFINDER);
#else
return false;
#endif
case FLIGHT_LOG_FIELD_CONDITION_RSSI:
return isRssiConfigured();
case FLIGHT_LOG_FIELD_CONDITION_NOT_LOGGING_EVERY_FRAME:
return blackboxConfig()->p_ratio != 1;
case FLIGHT_LOG_FIELD_CONDITION_ACC:
return sensors(SENSOR_ACC) && blackboxConfig()->record_acc;
case FLIGHT_LOG_FIELD_CONDITION_DEBUG:
return debugMode != DEBUG_NONE;
case FLIGHT_LOG_FIELD_CONDITION_NEVER:
return false;
default:
return false;
}
}
static void blackboxBuildConditionCache(void)
{
blackboxConditionCache = 0;
for (FlightLogFieldCondition cond = FLIGHT_LOG_FIELD_CONDITION_FIRST; cond <= FLIGHT_LOG_FIELD_CONDITION_LAST; cond++) {
if (testBlackboxConditionUncached(cond)) {
blackboxConditionCache |= 1 << cond;
}
}
}
static bool testBlackboxCondition(FlightLogFieldCondition condition)
{
return (blackboxConditionCache & (1 << condition)) != 0;
}
static void blackboxSetState(BlackboxState newState)
{
//Perform initial setup required for the new state
switch (newState) {
case BLACKBOX_STATE_PREPARE_LOG_FILE:
blackboxLoggedAnyFrames = false;
break;
case BLACKBOX_STATE_SEND_HEADER:
blackboxHeaderBudget = 0;
xmitState.headerIndex = 0;
xmitState.u.startTime = millis();
break;
case BLACKBOX_STATE_SEND_MAIN_FIELD_HEADER:
case BLACKBOX_STATE_SEND_GPS_G_HEADER:
case BLACKBOX_STATE_SEND_GPS_H_HEADER:
case BLACKBOX_STATE_SEND_SLOW_HEADER:
xmitState.headerIndex = 0;
xmitState.u.fieldIndex = -1;
break;
case BLACKBOX_STATE_SEND_SYSINFO:
xmitState.headerIndex = 0;
break;
case BLACKBOX_STATE_RUNNING:
blackboxSlowFrameIterationTimer = blackboxSInterval; //Force a slow frame to be written on the first iteration
break;
case BLACKBOX_STATE_SHUTTING_DOWN:
xmitState.u.startTime = millis();
break;
default:
;
}
blackboxState = newState;
}
static void writeIntraframe(void)
{
blackboxMainState_t *blackboxCurrent = blackboxHistory[0];
blackboxWrite('I');
blackboxWriteUnsignedVB(blackboxIteration);
blackboxWriteUnsignedVB(blackboxCurrent->time);
blackboxWriteSignedVBArray(blackboxCurrent->axisPID_P, XYZ_AXIS_COUNT);
blackboxWriteSignedVBArray(blackboxCurrent->axisPID_I, XYZ_AXIS_COUNT);
// Don't bother writing the current D term if the corresponding PID setting is zero
for (int x = 0; x < XYZ_AXIS_COUNT; x++) {
if (testBlackboxCondition(FLIGHT_LOG_FIELD_CONDITION_NONZERO_PID_D_0 + x)) {
blackboxWriteSignedVB(blackboxCurrent->axisPID_D[x]);
}
}
blackboxWriteSignedVBArray(blackboxCurrent->axisPID_F, XYZ_AXIS_COUNT);
// Write roll, pitch and yaw first:
blackboxWriteSigned16VBArray(blackboxCurrent->rcCommand, 3);
/*
* Write the throttle separately from the rest of the RC data as it's unsigned.
* Throttle lies in range [PWM_RANGE_MIN..PWM_RANGE_MAX]:
*/
blackboxWriteUnsignedVB(blackboxCurrent->rcCommand[THROTTLE]);
// Write setpoint roll, pitch, yaw, and throttle
blackboxWriteSigned16VBArray(blackboxCurrent->setpoint, 4);
if (testBlackboxCondition(FLIGHT_LOG_FIELD_CONDITION_VBAT)) {
/*
* Our voltage is expected to decrease over the course of the flight, so store our difference from
* the reference:
*
* Write 14 bits even if the number is negative (which would otherwise result in 32 bits)
*/
blackboxWriteUnsignedVB((vbatReference - blackboxCurrent->vbatLatest) & 0x3FFF);
}
if (testBlackboxCondition(FLIGHT_LOG_FIELD_CONDITION_AMPERAGE_ADC)) {
// 12bit value directly from ADC
blackboxWriteSignedVB(blackboxCurrent->amperageLatest);
}
#ifdef USE_MAG
if (testBlackboxCondition(FLIGHT_LOG_FIELD_CONDITION_MAG)) {
blackboxWriteSigned16VBArray(blackboxCurrent->magADC, XYZ_AXIS_COUNT);
}
#endif
#ifdef USE_BARO
if (testBlackboxCondition(FLIGHT_LOG_FIELD_CONDITION_BARO)) {
blackboxWriteSignedVB(blackboxCurrent->BaroAlt);
}
#endif
#ifdef USE_RANGEFINDER
if (testBlackboxCondition(FLIGHT_LOG_FIELD_CONDITION_RANGEFINDER)) {
blackboxWriteSignedVB(blackboxCurrent->surfaceRaw);
}
#endif
if (testBlackboxCondition(FLIGHT_LOG_FIELD_CONDITION_RSSI)) {
blackboxWriteUnsignedVB(blackboxCurrent->rssi);
}
blackboxWriteSigned16VBArray(blackboxCurrent->gyroADC, XYZ_AXIS_COUNT);
if (testBlackboxCondition(FLIGHT_LOG_FIELD_CONDITION_ACC)) {
blackboxWriteSigned16VBArray(blackboxCurrent->accADC, XYZ_AXIS_COUNT);
}
if (testBlackboxCondition(FLIGHT_LOG_FIELD_CONDITION_DEBUG)) {
blackboxWriteSigned16VBArray(blackboxCurrent->debug, DEBUG16_VALUE_COUNT);
}
//Motors can be below minimum output when disarmed, but that doesn't happen much
blackboxWriteUnsignedVB(blackboxCurrent->motor[0] - motorOutputLow);
//Motors tend to be similar to each other so use the first motor's value as a predictor of the others
const int motorCount = getMotorCount();
for (int x = 1; x < motorCount; x++) {
blackboxWriteSignedVB(blackboxCurrent->motor[x] - blackboxCurrent->motor[0]);
}
if (testBlackboxCondition(FLIGHT_LOG_FIELD_CONDITION_TRICOPTER)) {
//Assume the tail spends most of its time around the center
blackboxWriteSignedVB(blackboxCurrent->servo[5] - 1500);
}
//Rotate our history buffers:
//The current state becomes the new "before" state
blackboxHistory[1] = blackboxHistory[0];
//And since we have no other history, we also use it for the "before, before" state
blackboxHistory[2] = blackboxHistory[0];
//And advance the current state over to a blank space ready to be filled
blackboxHistory[0] = ((blackboxHistory[0] - blackboxHistoryRing + 1) % 3) + blackboxHistoryRing;
blackboxLoggedAnyFrames = true;
}
static void blackboxWriteMainStateArrayUsingAveragePredictor(int arrOffsetInHistory, int count)
{
int16_t *curr = (int16_t*) ((char*) (blackboxHistory[0]) + arrOffsetInHistory);
int16_t *prev1 = (int16_t*) ((char*) (blackboxHistory[1]) + arrOffsetInHistory);
int16_t *prev2 = (int16_t*) ((char*) (blackboxHistory[2]) + arrOffsetInHistory);
for (int i = 0; i < count; i++) {
// Predictor is the average of the previous two history states
int32_t predictor = (prev1[i] + prev2[i]) / 2;
blackboxWriteSignedVB(curr[i] - predictor);
}
}
static void writeInterframe(void)
{
blackboxMainState_t *blackboxCurrent = blackboxHistory[0];
blackboxMainState_t *blackboxLast = blackboxHistory[1];
blackboxWrite('P');
//No need to store iteration count since its delta is always 1
/*
* Since the difference between the difference between successive times will be nearly zero (due to consistent
* looptime spacing), use second-order differences.
*/
blackboxWriteSignedVB((int32_t) (blackboxHistory[0]->time - 2 * blackboxHistory[1]->time + blackboxHistory[2]->time));
int32_t deltas[8];
int32_t setpointDeltas[4];
arraySubInt32(deltas, blackboxCurrent->axisPID_P, blackboxLast->axisPID_P, XYZ_AXIS_COUNT);
blackboxWriteSignedVBArray(deltas, XYZ_AXIS_COUNT);
/*
* The PID I field changes very slowly, most of the time +-2, so use an encoding
* that can pack all three fields into one byte in that situation.
*/
arraySubInt32(deltas, blackboxCurrent->axisPID_I, blackboxLast->axisPID_I, XYZ_AXIS_COUNT);
blackboxWriteTag2_3S32(deltas);
/*
* The PID D term is frequently set to zero for yaw, which makes the result from the calculation
* always zero. So don't bother recording D results when PID D terms are zero.
*/
for (int x = 0; x < XYZ_AXIS_COUNT; x++) {
if (testBlackboxCondition(FLIGHT_LOG_FIELD_CONDITION_NONZERO_PID_D_0 + x)) {
blackboxWriteSignedVB(blackboxCurrent->axisPID_D[x] - blackboxLast->axisPID_D[x]);
}
}
arraySubInt32(deltas, blackboxCurrent->axisPID_F, blackboxLast->axisPID_F, XYZ_AXIS_COUNT);
blackboxWriteSignedVBArray(deltas, XYZ_AXIS_COUNT);
/*
* RC tends to stay the same or fairly small for many frames at a time, so use an encoding that
* can pack multiple values per byte:
*/
for (int x = 0; x < 4; x++) {
deltas[x] = blackboxCurrent->rcCommand[x] - blackboxLast->rcCommand[x];
setpointDeltas[x] = blackboxCurrent->setpoint[x] - blackboxLast->setpoint[x];
}
blackboxWriteTag8_4S16(deltas);
blackboxWriteTag8_4S16(setpointDeltas);
//Check for sensors that are updated periodically (so deltas are normally zero)
int optionalFieldCount = 0;
if (testBlackboxCondition(FLIGHT_LOG_FIELD_CONDITION_VBAT)) {
deltas[optionalFieldCount++] = (int32_t) blackboxCurrent->vbatLatest - blackboxLast->vbatLatest;
}
if (testBlackboxCondition(FLIGHT_LOG_FIELD_CONDITION_AMPERAGE_ADC)) {
deltas[optionalFieldCount++] = blackboxCurrent->amperageLatest - blackboxLast->amperageLatest;
}
#ifdef USE_MAG
if (testBlackboxCondition(FLIGHT_LOG_FIELD_CONDITION_MAG)) {
for (int x = 0; x < XYZ_AXIS_COUNT; x++) {
deltas[optionalFieldCount++] = blackboxCurrent->magADC[x] - blackboxLast->magADC[x];
}
}
#endif
#ifdef USE_BARO
if (testBlackboxCondition(FLIGHT_LOG_FIELD_CONDITION_BARO)) {
deltas[optionalFieldCount++] = blackboxCurrent->BaroAlt - blackboxLast->BaroAlt;
}
#endif
#ifdef USE_RANGEFINDER
if (testBlackboxCondition(FLIGHT_LOG_FIELD_CONDITION_RANGEFINDER)) {
deltas[optionalFieldCount++] = blackboxCurrent->surfaceRaw - blackboxLast->surfaceRaw;
}
#endif
if (testBlackboxCondition(FLIGHT_LOG_FIELD_CONDITION_RSSI)) {
deltas[optionalFieldCount++] = (int32_t) blackboxCurrent->rssi - blackboxLast->rssi;
}
blackboxWriteTag8_8SVB(deltas, optionalFieldCount);
//Since gyros, accs and motors are noisy, base their predictions on the average of the history:
blackboxWriteMainStateArrayUsingAveragePredictor(offsetof(blackboxMainState_t, gyroADC), XYZ_AXIS_COUNT);
if (testBlackboxCondition(FLIGHT_LOG_FIELD_CONDITION_ACC)) {
blackboxWriteMainStateArrayUsingAveragePredictor(offsetof(blackboxMainState_t, accADC), XYZ_AXIS_COUNT);
}
if (testBlackboxCondition(FLIGHT_LOG_FIELD_CONDITION_DEBUG)) {
blackboxWriteMainStateArrayUsingAveragePredictor(offsetof(blackboxMainState_t, debug), DEBUG16_VALUE_COUNT);
}
blackboxWriteMainStateArrayUsingAveragePredictor(offsetof(blackboxMainState_t, motor), getMotorCount());
if (testBlackboxCondition(FLIGHT_LOG_FIELD_CONDITION_TRICOPTER)) {
blackboxWriteSignedVB(blackboxCurrent->servo[5] - blackboxLast->servo[5]);
}
//Rotate our history buffers
blackboxHistory[2] = blackboxHistory[1];
blackboxHistory[1] = blackboxHistory[0];
blackboxHistory[0] = ((blackboxHistory[0] - blackboxHistoryRing + 1) % 3) + blackboxHistoryRing;
blackboxLoggedAnyFrames = true;
}
/* Write the contents of the global "slowHistory" to the log as an "S" frame. Because this data is logged so
* infrequently, delta updates are not reasonable, so we log independent frames. */
static void writeSlowFrame(void)
{
int32_t values[3];
blackboxWrite('S');
blackboxWriteUnsignedVB(slowHistory.flightModeFlags);
blackboxWriteUnsignedVB(slowHistory.stateFlags);
/*
* Most of the time these three values will be able to pack into one byte for us:
*/
values[0] = slowHistory.failsafePhase;
values[1] = slowHistory.rxSignalReceived ? 1 : 0;
values[2] = slowHistory.rxFlightChannelsValid ? 1 : 0;
blackboxWriteTag2_3S32(values);
blackboxSlowFrameIterationTimer = 0;
}
/**
* Load rarely-changing values from the FC into the given structure
*/
static void loadSlowState(blackboxSlowState_t *slow)
{
memcpy(&slow->flightModeFlags, &rcModeActivationMask, sizeof(slow->flightModeFlags)); //was flightModeFlags;
slow->stateFlags = stateFlags;
slow->failsafePhase = failsafePhase();
slow->rxSignalReceived = rxIsReceivingSignal();
slow->rxFlightChannelsValid = rxAreFlightChannelsValid();
}
/**
* If the data in the slow frame has changed, log a slow frame.
*
* If allowPeriodicWrite is true, the frame is also logged if it has been more than blackboxSInterval logging iterations
* since the field was last logged.
*/
STATIC_UNIT_TESTED bool writeSlowFrameIfNeeded(void)
{
// Write the slow frame peridocially so it can be recovered if we ever lose sync
bool shouldWrite = blackboxSlowFrameIterationTimer >= blackboxSInterval;
if (shouldWrite) {
loadSlowState(&slowHistory);
} else {
blackboxSlowState_t newSlowState;
loadSlowState(&newSlowState);
// Only write a slow frame if it was different from the previous state
if (memcmp(&newSlowState, &slowHistory, sizeof(slowHistory)) != 0) {
// Use the new state as our new history
memcpy(&slowHistory, &newSlowState, sizeof(slowHistory));
shouldWrite = true;
}
}
if (shouldWrite) {
writeSlowFrame();
}
return shouldWrite;
}
void blackboxValidateConfig(void)
{
// If we've chosen an unsupported device, change the device to serial
switch (blackboxConfig()->device) {
#ifdef USE_FLASHFS
case BLACKBOX_DEVICE_FLASH:
#endif
#ifdef USE_SDCARD
case BLACKBOX_DEVICE_SDCARD:
#endif
case BLACKBOX_DEVICE_SERIAL:
// Device supported, leave the setting alone
break;
default:
blackboxConfigMutable()->device = BLACKBOX_DEVICE_SERIAL;
}
}
static void blackboxResetIterationTimers(void)
{
blackboxIteration = 0;
blackboxLoopIndex = 0;
blackboxIFrameIndex = 0;
blackboxPFrameIndex = 0;
blackboxSlowFrameIterationTimer = 0;
}
/**
* Start Blackbox logging if it is not already running. Intended to be called upon arming.
*/
static void blackboxStart(void)
{
blackboxValidateConfig();
if (!blackboxDeviceOpen()) {
blackboxSetState(BLACKBOX_STATE_DISABLED);
return;
}
memset(&gpsHistory, 0, sizeof(gpsHistory));
blackboxHistory[0] = &blackboxHistoryRing[0];
blackboxHistory[1] = &blackboxHistoryRing[1];
blackboxHistory[2] = &blackboxHistoryRing[2];
vbatReference = getBatteryVoltageLatest();
//No need to clear the content of blackboxHistoryRing since our first frame will be an intra which overwrites it
/*
* We use conditional tests to decide whether or not certain fields should be logged. Since our headers
* must always agree with the logged data, the results of these tests must not change during logging. So
* cache those now.
*/
blackboxBuildConditionCache();
blackboxModeActivationConditionPresent = isModeActivationConditionPresent(BOXBLACKBOX);
blackboxResetIterationTimers();
/*
* Record the beeper's current idea of the last arming beep time, so that we can detect it changing when
* it finally plays the beep for this arming event.
*/
blackboxLastArmingBeep = getArmingBeepTimeMicros();
memcpy(&blackboxLastFlightModeFlags, &rcModeActivationMask, sizeof(blackboxLastFlightModeFlags)); // record startup status
blackboxSetState(BLACKBOX_STATE_PREPARE_LOG_FILE);
}
/**
* Begin Blackbox shutdown.
*/
void blackboxFinish(void)
{
switch (blackboxState) {
case BLACKBOX_STATE_DISABLED:
case BLACKBOX_STATE_STOPPED:
case BLACKBOX_STATE_SHUTTING_DOWN:
// We're already stopped/shutting down
break;
case BLACKBOX_STATE_RUNNING:
case BLACKBOX_STATE_PAUSED:
blackboxLogEvent(FLIGHT_LOG_EVENT_LOG_END, NULL);
FALLTHROUGH;
default:
blackboxSetState(BLACKBOX_STATE_SHUTTING_DOWN);
}
}
/**
* Test Motors Blackbox Logging
*/
static bool startedLoggingInTestMode = false;
static void startInTestMode(void)
{
if (!startedLoggingInTestMode) {
if (blackboxConfig()->device == BLACKBOX_DEVICE_SERIAL) {
serialPort_t *sharedBlackboxAndMspPort = findSharedSerialPort(FUNCTION_BLACKBOX, FUNCTION_MSP);
if (sharedBlackboxAndMspPort) {
return; // When in test mode, we cannot share the MSP and serial logger port!
}
}
blackboxStart();
startedLoggingInTestMode = true;
}
}
static void stopInTestMode(void)
{
if (startedLoggingInTestMode) {
blackboxFinish();
startedLoggingInTestMode = false;
}
}
/**
* We are going to monitor the MSP_SET_MOTOR target variables motor_disarmed[] for values other than minthrottle
* on reading a value (i.e. the user is testing the motors), then we enable test mode logging;
* we monitor when the values return to minthrottle and start a delay timer (5 seconds); if
* the test motors are left at minimum throttle for this delay timer, then we assume we are done testing and
* shutdown the logger.
*
* Of course, after the 5 seconds and shutdown of the logger, the system will be re-enabled to allow the
* test mode to trigger again; its just that the data will be in a second, third, fourth etc log file.
*/
static bool inMotorTestMode(void) {
static uint32_t resetTime = 0;
if (!ARMING_FLAG(ARMED) && areMotorsRunning()) {
resetTime = millis() + 5000; // add 5 seconds
return true;
} else {
// Monitor the duration at minimum
return (millis() < resetTime);
}
return false;
}
#ifdef USE_GPS
static void writeGPSHomeFrame(void)
{
blackboxWrite('H');
blackboxWriteSignedVB(GPS_home[0]);
blackboxWriteSignedVB(GPS_home[1]);
//TODO it'd be great if we could grab the GPS current time and write that too
gpsHistory.GPS_home[0] = GPS_home[0];
gpsHistory.GPS_home[1] = GPS_home[1];
}
static void writeGPSFrame(timeUs_t currentTimeUs)
{
blackboxWrite('G');
/*
* If we're logging every frame, then a GPS frame always appears just after a frame with the
* currentTime timestamp in the log, so the reader can just use that timestamp for the GPS frame.
*
* If we're not logging every frame, we need to store the time of this GPS frame.
*/
if (testBlackboxCondition(FLIGHT_LOG_FIELD_CONDITION_NOT_LOGGING_EVERY_FRAME)) {
// Predict the time of the last frame in the main log
blackboxWriteUnsignedVB(currentTimeUs - blackboxHistory[1]->time);
}
blackboxWriteUnsignedVB(gpsSol.numSat);
blackboxWriteSignedVB(gpsSol.llh.lat - gpsHistory.GPS_home[LAT]);
blackboxWriteSignedVB(gpsSol.llh.lon - gpsHistory.GPS_home[LON]);
blackboxWriteUnsignedVB(gpsSol.llh.altCm / 10); // was originally designed to transport meters in int16, but +-3276.7m is a good compromise
blackboxWriteUnsignedVB(gpsSol.groundSpeed);
blackboxWriteUnsignedVB(gpsSol.groundCourse);
gpsHistory.GPS_numSat = gpsSol.numSat;
gpsHistory.GPS_coord[LAT] = gpsSol.llh.lat;
gpsHistory.GPS_coord[LON] = gpsSol.llh.lon;
}
#endif
/**
* Fill the current state of the blackbox using values read from the flight controller
*/
static void loadMainState(timeUs_t currentTimeUs)
{
#ifndef UNIT_TEST
blackboxMainState_t *blackboxCurrent = blackboxHistory[0];
blackboxCurrent->time = currentTimeUs;
for (int i = 0; i < XYZ_AXIS_COUNT; i++) {
blackboxCurrent->axisPID_P[i] = pidData[i].P;
blackboxCurrent->axisPID_I[i] = pidData[i].I;
blackboxCurrent->axisPID_D[i] = pidData[i].D;
blackboxCurrent->axisPID_F[i] = pidData[i].F;
blackboxCurrent->gyroADC[i] = lrintf(gyro.gyroADCf[i]);
#if defined(USE_ACC)
blackboxCurrent->accADC[i] = lrintf(acc.accADC[i]);
#endif
#ifdef USE_MAG
blackboxCurrent->magADC[i] = mag.magADC[i];
#endif
}
for (int i = 0; i < 4; i++) {
blackboxCurrent->rcCommand[i] = lrintf(rcCommand[i]);
}
// log the currentPidSetpoint values applied to the PID controller
for (int i = 0; i < XYZ_AXIS_COUNT; i++) {
blackboxCurrent->setpoint[i] = lrintf(pidGetPreviousSetpoint(i));
}
// log the final throttle value used in the mixer
blackboxCurrent->setpoint[3] = lrintf(mixerGetLoggingThrottle() * 1000);
for (int i = 0; i < DEBUG16_VALUE_COUNT; i++) {
blackboxCurrent->debug[i] = debug[i];
}
const int motorCount = getMotorCount();
for (int i = 0; i < motorCount; i++) {
blackboxCurrent->motor[i] = motor[i];
}
blackboxCurrent->vbatLatest = getBatteryVoltageLatest();
blackboxCurrent->amperageLatest = getAmperageLatest();
#ifdef USE_BARO
blackboxCurrent->BaroAlt = baro.BaroAlt;
#endif
#ifdef USE_RANGEFINDER
// Store the raw sonar value without applying tilt correction
blackboxCurrent->surfaceRaw = rangefinderGetLatestAltitude();
#endif
blackboxCurrent->rssi = getRssi();
#ifdef USE_SERVOS
//Tail servo for tricopters
blackboxCurrent->servo[5] = servo[5];
#endif
#else
UNUSED(currentTimeUs);
#endif // UNIT_TEST
}
/**
* Transmit the header information for the given field definitions. Transmitted header lines look like:
*
* H Field I name:a,b,c
* H Field I predictor:0,1,2
*
* For all header types, provide a "mainFrameChar" which is the name for the field and will be used to refer to it in the
* header (e.g. P, I etc). For blackboxDeltaField_t fields, also provide deltaFrameChar, otherwise set this to zero.
*
* Provide an array 'conditions' of FlightLogFieldCondition enums if you want these conditions to decide whether a field
* should be included or not. Otherwise provide NULL for this parameter and NULL for secondCondition.
*
* Set xmitState.headerIndex to 0 and xmitState.u.fieldIndex to -1 before calling for the first time.
*
* secondFieldDefinition and secondCondition element pointers need to be provided in order to compute the stride of the
* fieldDefinition and secondCondition arrays.
*
* Returns true if there is still header left to transmit (so call again to continue transmission).
*/
static bool sendFieldDefinition(char mainFrameChar, char deltaFrameChar, const void *fieldDefinitions,
const void *secondFieldDefinition, int fieldCount, const uint8_t *conditions, const uint8_t *secondCondition)
{
const blackboxFieldDefinition_t *def;
unsigned int headerCount;
static bool needComma = false;
size_t definitionStride = (char*) secondFieldDefinition - (char*) fieldDefinitions;
size_t conditionsStride = (char*) secondCondition - (char*) conditions;
if (deltaFrameChar) {
headerCount = BLACKBOX_DELTA_FIELD_HEADER_COUNT;
} else {
headerCount = BLACKBOX_SIMPLE_FIELD_HEADER_COUNT;
}
/*
* We're chunking up the header data so we don't exceed our datarate. So we'll be called multiple times to transmit
* the whole header.
*/
// On our first call we need to print the name of the header and a colon
if (xmitState.u.fieldIndex == -1) {
if (xmitState.headerIndex >= headerCount) {
return false; //Someone probably called us again after we had already completed transmission
}
uint32_t charsToBeWritten = strlen("H Field x :") + strlen(blackboxFieldHeaderNames[xmitState.headerIndex]);
if (blackboxDeviceReserveBufferSpace(charsToBeWritten) != BLACKBOX_RESERVE_SUCCESS) {
return true; // Try again later
}
blackboxHeaderBudget -= blackboxPrintf("H Field %c %s:", xmitState.headerIndex >= BLACKBOX_SIMPLE_FIELD_HEADER_COUNT ? deltaFrameChar : mainFrameChar, blackboxFieldHeaderNames[xmitState.headerIndex]);
xmitState.u.fieldIndex++;
needComma = false;
}
// The longest we expect an integer to be as a string:
const uint32_t LONGEST_INTEGER_STRLEN = 2;
for (; xmitState.u.fieldIndex < fieldCount; xmitState.u.fieldIndex++) {
def = (const blackboxFieldDefinition_t*) ((const char*)fieldDefinitions + definitionStride * xmitState.u.fieldIndex);
if (!conditions || testBlackboxCondition(conditions[conditionsStride * xmitState.u.fieldIndex])) {
// First (over)estimate the length of the string we want to print
int32_t bytesToWrite = 1; // Leading comma
// The first header is a field name
if (xmitState.headerIndex == 0) {
bytesToWrite += strlen(def->name) + strlen("[]") + LONGEST_INTEGER_STRLEN;
} else {
//The other headers are integers
bytesToWrite += LONGEST_INTEGER_STRLEN;
}
// Now perform the write if the buffer is large enough
if (blackboxDeviceReserveBufferSpace(bytesToWrite) != BLACKBOX_RESERVE_SUCCESS) {
// Ran out of space!
return true;
}
blackboxHeaderBudget -= bytesToWrite;
if (needComma) {
blackboxWrite(',');
} else {
needComma = true;
}
// The first header is a field name
if (xmitState.headerIndex == 0) {
blackboxWriteString(def->name);
// Do we need to print an index in brackets after the name?
if (def->fieldNameIndex != -1) {
blackboxPrintf("[%d]", def->fieldNameIndex);
}
} else {
//The other headers are integers
blackboxPrintf("%d", def->arr[xmitState.headerIndex - 1]);
}
}
}
// Did we complete this line?
if (xmitState.u.fieldIndex == fieldCount && blackboxDeviceReserveBufferSpace(1) == BLACKBOX_RESERVE_SUCCESS) {
blackboxHeaderBudget--;
blackboxWrite('\n');
xmitState.headerIndex++;
xmitState.u.fieldIndex = -1;
}
return xmitState.headerIndex < headerCount;
}
// Buf must be at least FORMATTED_DATE_TIME_BUFSIZE
STATIC_UNIT_TESTED char *blackboxGetStartDateTime(char *buf)
{
#ifdef USE_RTC_TIME
dateTime_t dt;
// rtcGetDateTime will fill dt with 0000-01-01T00:00:00
// when time is not known.
rtcGetDateTime(&dt);
dateTimeFormatLocal(buf, &dt);
#else
buf = "0000-01-01T00:00:00.000";
#endif
return buf;
}
#ifndef BLACKBOX_PRINT_HEADER_LINE
#define BLACKBOX_PRINT_HEADER_LINE(name, format, ...) case __COUNTER__: \
blackboxPrintfHeaderLine(name, format, __VA_ARGS__); \
break;
#define BLACKBOX_PRINT_HEADER_LINE_CUSTOM(...) case __COUNTER__: \
{__VA_ARGS__}; \
break;
#endif
/**
* Transmit a portion of the system information headers. Call the first time with xmitState.headerIndex == 0. Returns
* true iff transmission is complete, otherwise call again later to continue transmission.
*/
static bool blackboxWriteSysinfo(void)
{
#ifndef UNIT_TEST
const uint16_t motorOutputLowInt = lrintf(motorOutputLow);
const uint16_t motorOutputHighInt = lrintf(motorOutputHigh);
// Make sure we have enough room in the buffer for our longest line (as of this writing, the "Firmware date" line)
if (blackboxDeviceReserveBufferSpace(64) != BLACKBOX_RESERVE_SUCCESS) {
return false;
}
char buf[FORMATTED_DATE_TIME_BUFSIZE];
#ifdef USE_RC_SMOOTHING_FILTER
rcSmoothingFilter_t *rcSmoothingData = getRcSmoothingData();
#endif
const controlRateConfig_t *currentControlRateProfile = controlRateProfiles(systemConfig()->activeRateProfile);
switch (xmitState.headerIndex) {
BLACKBOX_PRINT_HEADER_LINE("Firmware type", "%s", "Cleanflight");
BLACKBOX_PRINT_HEADER_LINE("Firmware revision", "%s %s (%s) %s", FC_FIRMWARE_NAME, FC_VERSION_STRING, shortGitRevision, targetName);
BLACKBOX_PRINT_HEADER_LINE("Firmware date", "%s %s", buildDate, buildTime);
BLACKBOX_PRINT_HEADER_LINE("Log start datetime", "%s", blackboxGetStartDateTime(buf));
BLACKBOX_PRINT_HEADER_LINE("Craft name", "%s", pilotConfig()->name);
BLACKBOX_PRINT_HEADER_LINE("I interval", "%d", blackboxIInterval);
BLACKBOX_PRINT_HEADER_LINE("P interval", "%d", blackboxPInterval);
BLACKBOX_PRINT_HEADER_LINE("P ratio", "%d", blackboxConfig()->p_ratio);
BLACKBOX_PRINT_HEADER_LINE("minthrottle", "%d", motorConfig()->minthrottle);
BLACKBOX_PRINT_HEADER_LINE("maxthrottle", "%d", motorConfig()->maxthrottle);
BLACKBOX_PRINT_HEADER_LINE("gyro_scale","0x%x", castFloatBytesToInt(1.0f));
BLACKBOX_PRINT_HEADER_LINE("motorOutput", "%d,%d", motorOutputLowInt,motorOutputHighInt);
#if defined(USE_ACC)
BLACKBOX_PRINT_HEADER_LINE("acc_1G", "%u", acc.dev.acc_1G);
#endif
BLACKBOX_PRINT_HEADER_LINE_CUSTOM(
if (testBlackboxCondition(FLIGHT_LOG_FIELD_CONDITION_VBAT)) {
blackboxPrintfHeaderLine("vbat_scale", "%u", voltageSensorADCConfig(VOLTAGE_SENSOR_ADC_VBAT)->vbatscale);
} else {
xmitState.headerIndex += 2; // Skip the next two vbat fields too
}
);
BLACKBOX_PRINT_HEADER_LINE("vbatcellvoltage", "%u,%u,%u", batteryConfig()->vbatmincellvoltage,
batteryConfig()->vbatwarningcellvoltage,
batteryConfig()->vbatmaxcellvoltage);
BLACKBOX_PRINT_HEADER_LINE("vbatref", "%u", vbatReference);
BLACKBOX_PRINT_HEADER_LINE_CUSTOM(
if (batteryConfig()->currentMeterSource == CURRENT_METER_ADC) {
blackboxPrintfHeaderLine("currentSensor", "%d,%d",currentSensorADCConfig()->offset, currentSensorADCConfig()->scale);
}
);
BLACKBOX_PRINT_HEADER_LINE("looptime", "%d", gyro.targetLooptime);
BLACKBOX_PRINT_HEADER_LINE("gyro_sync_denom", "%d", gyroConfig()->gyro_sync_denom);
BLACKBOX_PRINT_HEADER_LINE("pid_process_denom", "%d", pidConfig()->pid_process_denom);
BLACKBOX_PRINT_HEADER_LINE("thr_mid", "%d", currentControlRateProfile->thrMid8);
BLACKBOX_PRINT_HEADER_LINE("thr_expo", "%d", currentControlRateProfile->thrExpo8);
BLACKBOX_PRINT_HEADER_LINE("tpa_rate", "%d", currentControlRateProfile->dynThrPID);
BLACKBOX_PRINT_HEADER_LINE("tpa_breakpoint", "%d", currentControlRateProfile->tpa_breakpoint);
BLACKBOX_PRINT_HEADER_LINE("rc_rates", "%d,%d,%d", currentControlRateProfile->rcRates[ROLL],
currentControlRateProfile->rcRates[PITCH],
currentControlRateProfile->rcRates[YAW]);
BLACKBOX_PRINT_HEADER_LINE("rc_expo", "%d,%d,%d", currentControlRateProfile->rcExpo[ROLL],
currentControlRateProfile->rcExpo[PITCH],
currentControlRateProfile->rcExpo[YAW]);
BLACKBOX_PRINT_HEADER_LINE("rates", "%d,%d,%d", currentControlRateProfile->rates[ROLL],
currentControlRateProfile->rates[PITCH],
currentControlRateProfile->rates[YAW]);
BLACKBOX_PRINT_HEADER_LINE("rate_limits", "%d,%d,%d", currentControlRateProfile->rate_limit[ROLL],
currentControlRateProfile->rate_limit[PITCH],
currentControlRateProfile->rate_limit[YAW]);
BLACKBOX_PRINT_HEADER_LINE("rollPID", "%d,%d,%d", currentPidProfile->pid[PID_ROLL].P,
currentPidProfile->pid[PID_ROLL].I,
currentPidProfile->pid[PID_ROLL].D);
BLACKBOX_PRINT_HEADER_LINE("pitchPID", "%d,%d,%d", currentPidProfile->pid[PID_PITCH].P,
currentPidProfile->pid[PID_PITCH].I,
currentPidProfile->pid[PID_PITCH].D);
BLACKBOX_PRINT_HEADER_LINE("yawPID", "%d,%d,%d", currentPidProfile->pid[PID_YAW].P,
currentPidProfile->pid[PID_YAW].I,
currentPidProfile->pid[PID_YAW].D);
BLACKBOX_PRINT_HEADER_LINE("levelPID", "%d,%d,%d", currentPidProfile->pid[PID_LEVEL].P,
currentPidProfile->pid[PID_LEVEL].I,
currentPidProfile->pid[PID_LEVEL].D);
BLACKBOX_PRINT_HEADER_LINE("magPID", "%d", currentPidProfile->pid[PID_MAG].P);
#ifdef USE_D_MIN
BLACKBOX_PRINT_HEADER_LINE("d_min", "%d,%d,%d", currentPidProfile->d_min[ROLL],
currentPidProfile->d_min[PITCH],
currentPidProfile->d_min[YAW]);
BLACKBOX_PRINT_HEADER_LINE("d_min_gain", "%d", currentPidProfile->d_min_gain);
BLACKBOX_PRINT_HEADER_LINE("d_min_advance", "%d", currentPidProfile->d_min_advance);
#endif
BLACKBOX_PRINT_HEADER_LINE("dterm_filter_type", "%d", currentPidProfile->dterm_filter_type);
BLACKBOX_PRINT_HEADER_LINE("dterm_lowpass_hz", "%d", currentPidProfile->dterm_lowpass_hz);
#ifdef USE_DYN_LPF
BLACKBOX_PRINT_HEADER_LINE("dterm_lowpass_dyn_hz", "%d,%d", currentPidProfile->dyn_lpf_dterm_min_hz,
currentPidProfile->dyn_lpf_dterm_max_hz);
#endif
BLACKBOX_PRINT_HEADER_LINE("dterm_filter2_type", "%d", currentPidProfile->dterm_filter2_type);
BLACKBOX_PRINT_HEADER_LINE("dterm_lowpass2_hz", "%d", currentPidProfile->dterm_lowpass2_hz);
BLACKBOX_PRINT_HEADER_LINE("yaw_lowpass_hz", "%d", currentPidProfile->yaw_lowpass_hz);
BLACKBOX_PRINT_HEADER_LINE("dterm_notch_hz", "%d", currentPidProfile->dterm_notch_hz);
BLACKBOX_PRINT_HEADER_LINE("dterm_notch_cutoff", "%d", currentPidProfile->dterm_notch_cutoff);
BLACKBOX_PRINT_HEADER_LINE("iterm_windup", "%d", currentPidProfile->itermWindupPointPercent);
BLACKBOX_PRINT_HEADER_LINE("vbat_pid_gain", "%d", currentPidProfile->vbatPidCompensation);
BLACKBOX_PRINT_HEADER_LINE("pidAtMinThrottle", "%d", currentPidProfile->pidAtMinThrottle);
// Betaflight PID controller parameters
BLACKBOX_PRINT_HEADER_LINE("anti_gravity_mode", "%d", currentPidProfile->antiGravityMode);
BLACKBOX_PRINT_HEADER_LINE("anti_gravity_threshold", "%d", currentPidProfile->itermThrottleThreshold);
BLACKBOX_PRINT_HEADER_LINE("anti_gravity_gain", "%d", currentPidProfile->itermAcceleratorGain);
#ifdef USE_ABSOLUTE_CONTROL
BLACKBOX_PRINT_HEADER_LINE("abs_control_gain", "%d", currentPidProfile->abs_control_gain);
#endif
#ifdef USE_INTEGRATED_YAW_CONTROL
BLACKBOX_PRINT_HEADER_LINE("use_integrated_yaw", "%d", currentPidProfile->use_integrated_yaw);
#endif
BLACKBOX_PRINT_HEADER_LINE("feedforward_transition", "%d", currentPidProfile->feedForwardTransition);
BLACKBOX_PRINT_HEADER_LINE("feedforward_weight", "%d,%d,%d", currentPidProfile->pid[PID_ROLL].F,
currentPidProfile->pid[PID_PITCH].F,
currentPidProfile->pid[PID_YAW].F);
BLACKBOX_PRINT_HEADER_LINE("acc_limit_yaw", "%d", currentPidProfile->yawRateAccelLimit);
BLACKBOX_PRINT_HEADER_LINE("acc_limit", "%d", currentPidProfile->rateAccelLimit);
BLACKBOX_PRINT_HEADER_LINE("pidsum_limit", "%d", currentPidProfile->pidSumLimit);
BLACKBOX_PRINT_HEADER_LINE("pidsum_limit_yaw", "%d", currentPidProfile->pidSumLimitYaw);
// End of Betaflight controller parameters
BLACKBOX_PRINT_HEADER_LINE("deadband", "%d", rcControlsConfig()->deadband);
BLACKBOX_PRINT_HEADER_LINE("yaw_deadband", "%d", rcControlsConfig()->yaw_deadband);
BLACKBOX_PRINT_HEADER_LINE("gyro_hardware_lpf", "%d", gyroConfig()->gyro_hardware_lpf);
BLACKBOX_PRINT_HEADER_LINE("gyro_lowpass_type", "%d", gyroConfig()->gyro_lowpass_type);
BLACKBOX_PRINT_HEADER_LINE("gyro_lowpass_hz", "%d", gyroConfig()->gyro_lowpass_hz);
#ifdef USE_DYN_LPF
BLACKBOX_PRINT_HEADER_LINE("gyro_lowpass_dyn_hz", "%d,%d", gyroConfig()->dyn_lpf_gyro_min_hz,
gyroConfig()->dyn_lpf_gyro_max_hz);
#endif
BLACKBOX_PRINT_HEADER_LINE("gyro_lowpass2_type", "%d", gyroConfig()->gyro_lowpass2_type);
BLACKBOX_PRINT_HEADER_LINE("gyro_lowpass2_hz", "%d", gyroConfig()->gyro_lowpass2_hz);
BLACKBOX_PRINT_HEADER_LINE("gyro_notch_hz", "%d,%d", gyroConfig()->gyro_soft_notch_hz_1,
gyroConfig()->gyro_soft_notch_hz_2);
BLACKBOX_PRINT_HEADER_LINE("gyro_notch_cutoff", "%d,%d", gyroConfig()->gyro_soft_notch_cutoff_1,
gyroConfig()->gyro_soft_notch_cutoff_2);
#if defined(USE_ACC)
BLACKBOX_PRINT_HEADER_LINE("acc_lpf_hz", "%d", (int)(accelerometerConfig()->acc_lpf_hz * 100.0f));
BLACKBOX_PRINT_HEADER_LINE("acc_hardware", "%d", accelerometerConfig()->acc_hardware);
#endif
#ifdef USE_BARO
BLACKBOX_PRINT_HEADER_LINE("baro_hardware", "%d", barometerConfig()->baro_hardware);
#endif
#ifdef USE_MAG
BLACKBOX_PRINT_HEADER_LINE("mag_hardware", "%d", compassConfig()->mag_hardware);
#endif
BLACKBOX_PRINT_HEADER_LINE("gyro_cal_on_first_arm", "%d", armingConfig()->gyro_cal_on_first_arm);
BLACKBOX_PRINT_HEADER_LINE("rc_interpolation", "%d", rxConfig()->rcInterpolation);
BLACKBOX_PRINT_HEADER_LINE("rc_interpolation_interval", "%d", rxConfig()->rcInterpolationInterval);
BLACKBOX_PRINT_HEADER_LINE("rc_interpolation_channels", "%d", rxConfig()->rcInterpolationChannels);
BLACKBOX_PRINT_HEADER_LINE("airmode_activate_throttle", "%d", rxConfig()->airModeActivateThreshold);
BLACKBOX_PRINT_HEADER_LINE("serialrx_provider", "%d", rxConfig()->serialrx_provider);
BLACKBOX_PRINT_HEADER_LINE("use_unsynced_pwm", "%d", motorConfig()->dev.useUnsyncedPwm);
BLACKBOX_PRINT_HEADER_LINE("motor_pwm_protocol", "%d", motorConfig()->dev.motorPwmProtocol);
BLACKBOX_PRINT_HEADER_LINE("motor_pwm_rate", "%d", motorConfig()->dev.motorPwmRate);
BLACKBOX_PRINT_HEADER_LINE("dshot_idle_value", "%d", motorConfig()->digitalIdleOffsetValue);
BLACKBOX_PRINT_HEADER_LINE("debug_mode", "%d", debugMode);
BLACKBOX_PRINT_HEADER_LINE("features", "%d", featureConfig()->enabledFeatures);
#ifdef USE_RC_SMOOTHING_FILTER
BLACKBOX_PRINT_HEADER_LINE("rc_smoothing_type", "%d", rcSmoothingData->inputFilterType);
BLACKBOX_PRINT_HEADER_LINE("rc_smoothing_debug_axis", "%d", rcSmoothingData->debugAxis);
BLACKBOX_PRINT_HEADER_LINE("rc_smoothing_cutoffs", "%d, %d", rcSmoothingData->inputCutoffSetting,
rcSmoothingData->derivativeCutoffSetting);
BLACKBOX_PRINT_HEADER_LINE("rc_smoothing_auto_factor", "%d", rcSmoothingData->autoSmoothnessFactor);
BLACKBOX_PRINT_HEADER_LINE("rc_smoothing_filter_type", "%d, %d", rcSmoothingData->inputFilterType,
rcSmoothingData->derivativeFilterType);
BLACKBOX_PRINT_HEADER_LINE("rc_smoothing_active_cutoffs", "%d, %d", rcSmoothingData->inputCutoffFrequency,
rcSmoothingData->derivativeCutoffFrequency);
BLACKBOX_PRINT_HEADER_LINE("rc_smoothing_rx_average", "%d", rcSmoothingData->averageFrameTimeUs);
#endif // USE_RC_SMOOTHING_FILTER
default:
return true;
}
xmitState.headerIndex++;
#endif // UNIT_TEST
return false;
}
/**
* Write the given event to the log immediately
*/
void blackboxLogEvent(FlightLogEvent event, flightLogEventData_t *data)
{
// Only allow events to be logged after headers have been written
if (!(blackboxState == BLACKBOX_STATE_RUNNING || blackboxState == BLACKBOX_STATE_PAUSED)) {
return;
}
//Shared header for event frames
blackboxWrite('E');
blackboxWrite(event);
//Now serialize the data for this specific frame type
switch (event) {
case FLIGHT_LOG_EVENT_SYNC_BEEP:
blackboxWriteUnsignedVB(data->syncBeep.time);
break;
case FLIGHT_LOG_EVENT_FLIGHTMODE: // New flightmode flags write
blackboxWriteUnsignedVB(data->flightMode.flags);
blackboxWriteUnsignedVB(data->flightMode.lastFlags);
break;
case FLIGHT_LOG_EVENT_INFLIGHT_ADJUSTMENT:
if (data->inflightAdjustment.floatFlag) {
blackboxWrite(data->inflightAdjustment.adjustmentFunction + FLIGHT_LOG_EVENT_INFLIGHT_ADJUSTMENT_FUNCTION_FLOAT_VALUE_FLAG);
blackboxWriteFloat(data->inflightAdjustment.newFloatValue);
} else {
blackboxWrite(data->inflightAdjustment.adjustmentFunction);
blackboxWriteSignedVB(data->inflightAdjustment.newValue);
}
break;
case FLIGHT_LOG_EVENT_LOGGING_RESUME:
blackboxWriteUnsignedVB(data->loggingResume.logIteration);
blackboxWriteUnsignedVB(data->loggingResume.currentTime);
break;
case FLIGHT_LOG_EVENT_LOG_END:
blackboxWriteString("End of log");
blackboxWrite(0);
break;
}
}
/* If an arming beep has played since it was last logged, write the time of the arming beep to the log as a synchronization point */
static void blackboxCheckAndLogArmingBeep(void)
{
// Use != so that we can still detect a change if the counter wraps
if (getArmingBeepTimeMicros() != blackboxLastArmingBeep) {
blackboxLastArmingBeep = getArmingBeepTimeMicros();
flightLogEvent_syncBeep_t eventData;
eventData.time = blackboxLastArmingBeep;
blackboxLogEvent(FLIGHT_LOG_EVENT_SYNC_BEEP, (flightLogEventData_t *)&eventData);
}
}
/* monitor the flight mode event status and trigger an event record if the state changes */
static void blackboxCheckAndLogFlightMode(void)
{
// Use != so that we can still detect a change if the counter wraps
if (memcmp(&rcModeActivationMask, &blackboxLastFlightModeFlags, sizeof(blackboxLastFlightModeFlags))) {
flightLogEvent_flightMode_t eventData; // Add new data for current flight mode flags
eventData.lastFlags = blackboxLastFlightModeFlags;
memcpy(&blackboxLastFlightModeFlags, &rcModeActivationMask, sizeof(blackboxLastFlightModeFlags));
memcpy(&eventData.flags, &rcModeActivationMask, sizeof(eventData.flags));
blackboxLogEvent(FLIGHT_LOG_EVENT_FLIGHTMODE, (flightLogEventData_t *)&eventData);
}
}
STATIC_UNIT_TESTED bool blackboxShouldLogPFrame(void)
{
return blackboxPFrameIndex == 0 && blackboxConfig()->p_ratio != 0;
}
STATIC_UNIT_TESTED bool blackboxShouldLogIFrame(void)
{
return blackboxLoopIndex == 0;
}
/*
* If the GPS home point has been updated, or every 128 I-frames (~10 seconds), write the
* GPS home position.
*
* We write it periodically so that if one Home Frame goes missing, the GPS coordinates can
* still be interpreted correctly.
*/
#ifdef USE_GPS
STATIC_UNIT_TESTED bool blackboxShouldLogGpsHomeFrame(void)
{
if (GPS_home[0] != gpsHistory.GPS_home[0] || GPS_home[1] != gpsHistory.GPS_home[1]
|| (blackboxPFrameIndex == blackboxIInterval / 2 && blackboxIFrameIndex % 128 == 0)) {
return true;
}
return false;
}
#endif // GPS
// Called once every FC loop in order to keep track of how many FC loop iterations have passed
STATIC_UNIT_TESTED void blackboxAdvanceIterationTimers(void)
{
++blackboxSlowFrameIterationTimer;
++blackboxIteration;
if (++blackboxLoopIndex >= blackboxIInterval) {
blackboxLoopIndex = 0;
blackboxIFrameIndex++;
blackboxPFrameIndex = 0;
} else if (++blackboxPFrameIndex >= blackboxPInterval) {
blackboxPFrameIndex = 0;
}
}
// Called once every FC loop in order to log the current state
STATIC_UNIT_TESTED void blackboxLogIteration(timeUs_t currentTimeUs)
{
// Write a keyframe every blackboxIInterval frames so we can resynchronise upon missing frames
if (blackboxShouldLogIFrame()) {
/*
* Don't log a slow frame if the slow data didn't change ("I" frames are already large enough without adding
* an additional item to write at the same time). Unless we're *only* logging "I" frames, then we have no choice.
*/
if (blackboxIsOnlyLoggingIntraframes()) {
writeSlowFrameIfNeeded();
}
loadMainState(currentTimeUs);
writeIntraframe();
} else {
blackboxCheckAndLogArmingBeep();
blackboxCheckAndLogFlightMode(); // Check for FlightMode status change event
if (blackboxShouldLogPFrame()) {
/*
* We assume that slow frames are only interesting in that they aid the interpretation of the main data stream.
* So only log slow frames during loop iterations where we log a main frame.
*/
writeSlowFrameIfNeeded();
loadMainState(currentTimeUs);
writeInterframe();
}
#ifdef USE_GPS
if (featureIsEnabled(FEATURE_GPS)) {
if (blackboxShouldLogGpsHomeFrame()) {
writeGPSHomeFrame();
writeGPSFrame(currentTimeUs);
} else if (gpsSol.numSat != gpsHistory.GPS_numSat
|| gpsSol.llh.lat != gpsHistory.GPS_coord[LAT]
|| gpsSol.llh.lon != gpsHistory.GPS_coord[LON]) {
//We could check for velocity changes as well but I doubt it changes independent of position
writeGPSFrame(currentTimeUs);
}
}
#endif
}
//Flush every iteration so that our runtime variance is minimized
blackboxDeviceFlush();
}
/**
* Call each flight loop iteration to perform blackbox logging.
*/
void blackboxUpdate(timeUs_t currentTimeUs)
{
switch (blackboxState) {
case BLACKBOX_STATE_STOPPED:
if (ARMING_FLAG(ARMED)) {
blackboxOpen();
blackboxStart();
}
#ifdef USE_FLASHFS
if (IS_RC_MODE_ACTIVE(BOXBLACKBOXERASE)) {
blackboxSetState(BLACKBOX_STATE_START_ERASE);
}
#endif
break;
case BLACKBOX_STATE_PREPARE_LOG_FILE:
if (blackboxDeviceBeginLog()) {
blackboxSetState(BLACKBOX_STATE_SEND_HEADER);
}
break;
case BLACKBOX_STATE_SEND_HEADER:
blackboxReplenishHeaderBudget();
//On entry of this state, xmitState.headerIndex is 0 and startTime is intialised
/*
* Once the UART has had time to init, transmit the header in chunks so we don't overflow its transmit
* buffer, overflow the OpenLog's buffer, or keep the main loop busy for too long.
*/
if (millis() > xmitState.u.startTime + 100) {
if (blackboxDeviceReserveBufferSpace(BLACKBOX_TARGET_HEADER_BUDGET_PER_ITERATION) == BLACKBOX_RESERVE_SUCCESS) {
for (int i = 0; i < BLACKBOX_TARGET_HEADER_BUDGET_PER_ITERATION && blackboxHeader[xmitState.headerIndex] != '\0'; i++, xmitState.headerIndex++) {
blackboxWrite(blackboxHeader[xmitState.headerIndex]);
blackboxHeaderBudget--;
}
if (blackboxHeader[xmitState.headerIndex] == '\0') {
blackboxSetState(BLACKBOX_STATE_SEND_MAIN_FIELD_HEADER);
}
}
}
break;
case BLACKBOX_STATE_SEND_MAIN_FIELD_HEADER:
blackboxReplenishHeaderBudget();
//On entry of this state, xmitState.headerIndex is 0 and xmitState.u.fieldIndex is -1
if (!sendFieldDefinition('I', 'P', blackboxMainFields, blackboxMainFields + 1, ARRAYLEN(blackboxMainFields),
&blackboxMainFields[0].condition, &blackboxMainFields[1].condition)) {
#ifdef USE_GPS
if (featureIsEnabled(FEATURE_GPS)) {
blackboxSetState(BLACKBOX_STATE_SEND_GPS_H_HEADER);
} else
#endif
blackboxSetState(BLACKBOX_STATE_SEND_SLOW_HEADER);
}
break;
#ifdef USE_GPS
case BLACKBOX_STATE_SEND_GPS_H_HEADER:
blackboxReplenishHeaderBudget();
//On entry of this state, xmitState.headerIndex is 0 and xmitState.u.fieldIndex is -1
if (!sendFieldDefinition('H', 0, blackboxGpsHFields, blackboxGpsHFields + 1, ARRAYLEN(blackboxGpsHFields),
NULL, NULL)) {
blackboxSetState(BLACKBOX_STATE_SEND_GPS_G_HEADER);
}
break;
case BLACKBOX_STATE_SEND_GPS_G_HEADER:
blackboxReplenishHeaderBudget();
//On entry of this state, xmitState.headerIndex is 0 and xmitState.u.fieldIndex is -1
if (!sendFieldDefinition('G', 0, blackboxGpsGFields, blackboxGpsGFields + 1, ARRAYLEN(blackboxGpsGFields),
&blackboxGpsGFields[0].condition, &blackboxGpsGFields[1].condition)) {
blackboxSetState(BLACKBOX_STATE_SEND_SLOW_HEADER);
}
break;
#endif
case BLACKBOX_STATE_SEND_SLOW_HEADER:
blackboxReplenishHeaderBudget();
//On entry of this state, xmitState.headerIndex is 0 and xmitState.u.fieldIndex is -1
if (!sendFieldDefinition('S', 0, blackboxSlowFields, blackboxSlowFields + 1, ARRAYLEN(blackboxSlowFields),
NULL, NULL)) {
blackboxSetState(BLACKBOX_STATE_SEND_SYSINFO);
}
break;
case BLACKBOX_STATE_SEND_SYSINFO:
blackboxReplenishHeaderBudget();
//On entry of this state, xmitState.headerIndex is 0
//Keep writing chunks of the system info headers until it returns true to signal completion
if (blackboxWriteSysinfo()) {
/*
* Wait for header buffers to drain completely before data logging begins to ensure reliable header delivery
* (overflowing circular buffers causes all data to be discarded, so the first few logged iterations
* could wipe out the end of the header if we weren't careful)
*/
if (blackboxDeviceFlushForce()) {
blackboxSetState(BLACKBOX_STATE_RUNNING);
}
}
break;
case BLACKBOX_STATE_PAUSED:
// Only allow resume to occur during an I-frame iteration, so that we have an "I" base to work from
if (IS_RC_MODE_ACTIVE(BOXBLACKBOX) && blackboxShouldLogIFrame()) {
// Write a log entry so the decoder is aware that our large time/iteration skip is intended
flightLogEvent_loggingResume_t resume;
resume.logIteration = blackboxIteration;
resume.currentTime = currentTimeUs;
blackboxLogEvent(FLIGHT_LOG_EVENT_LOGGING_RESUME, (flightLogEventData_t *) &resume);
blackboxSetState(BLACKBOX_STATE_RUNNING);
blackboxLogIteration(currentTimeUs);
}
// Keep the logging timers ticking so our log iteration continues to advance
blackboxAdvanceIterationTimers();
break;
case BLACKBOX_STATE_RUNNING:
// On entry to this state, blackboxIteration, blackboxPFrameIndex and blackboxIFrameIndex are reset to 0
// Prevent the Pausing of the log on the mode switch if in Motor Test Mode
if (blackboxModeActivationConditionPresent && !IS_RC_MODE_ACTIVE(BOXBLACKBOX) && !startedLoggingInTestMode) {
blackboxSetState(BLACKBOX_STATE_PAUSED);
} else {
blackboxLogIteration(currentTimeUs);
}
blackboxAdvanceIterationTimers();
break;
case BLACKBOX_STATE_SHUTTING_DOWN:
//On entry of this state, startTime is set
/*
* Wait for the log we've transmitted to make its way to the logger before we release the serial port,
* since releasing the port clears the Tx buffer.
*
* Don't wait longer than it could possibly take if something funky happens.
*/
if (blackboxDeviceEndLog(blackboxLoggedAnyFrames) && (millis() > xmitState.u.startTime + BLACKBOX_SHUTDOWN_TIMEOUT_MILLIS || blackboxDeviceFlushForce())) {
blackboxDeviceClose();
blackboxSetState(BLACKBOX_STATE_STOPPED);
}
break;
#ifdef USE_FLASHFS
case BLACKBOX_STATE_START_ERASE:
blackboxEraseAll();
blackboxSetState(BLACKBOX_STATE_ERASING);
beeper(BEEPER_BLACKBOX_ERASE);
break;
case BLACKBOX_STATE_ERASING:
if (isBlackboxErased()) {
//Done erasing
blackboxSetState(BLACKBOX_STATE_ERASED);
beeper(BEEPER_BLACKBOX_ERASE);
}
break;
case BLACKBOX_STATE_ERASED:
if (!IS_RC_MODE_ACTIVE(BOXBLACKBOXERASE)) {
blackboxSetState(BLACKBOX_STATE_STOPPED);
}
break;
#endif
default:
break;
}
// Did we run out of room on the device? Stop!
if (isBlackboxDeviceFull()) {
#ifdef USE_FLASHFS
if (blackboxState != BLACKBOX_STATE_ERASING
&& blackboxState != BLACKBOX_STATE_START_ERASE
&& blackboxState != BLACKBOX_STATE_ERASED)
#endif
{
blackboxSetState(BLACKBOX_STATE_STOPPED);
// ensure we reset the test mode flag if we stop due to full memory card
if (startedLoggingInTestMode) {
startedLoggingInTestMode = false;
}
}
} else { // Only log in test mode if there is room!
switch (blackboxConfig()->mode) {
case BLACKBOX_MODE_MOTOR_TEST:
// Handle Motor Test Mode
if (inMotorTestMode()) {
if (blackboxState==BLACKBOX_STATE_STOPPED) {
startInTestMode();
}
} else {
if (blackboxState!=BLACKBOX_STATE_STOPPED) {
stopInTestMode();
}
}
break;
case BLACKBOX_MODE_ALWAYS_ON:
if (blackboxState==BLACKBOX_STATE_STOPPED) {
startInTestMode();
}
break;
case BLACKBOX_MODE_NORMAL:
default:
break;
}
}
}
int blackboxCalculatePDenom(int rateNum, int rateDenom)
{
return blackboxIInterval * rateNum / rateDenom;
}
uint8_t blackboxGetRateDenom(void)
{
return blackboxPInterval;
}
/**
* Call during system startup to initialize the blackbox.
*/
void blackboxInit(void)
{
blackboxResetIterationTimers();
// an I-frame is written every 32ms
// blackboxUpdate() is run in synchronisation with the PID loop
// targetPidLooptime is 1000 for 1kHz loop, 500 for 2kHz loop etc, targetPidLooptime is rounded for short looptimes
if (targetPidLooptime == 31) { // rounded from 31.25us
blackboxIInterval = 1024;
} else if (targetPidLooptime == 63) { // rounded from 62.5us
blackboxIInterval = 512;
} else {
blackboxIInterval = (uint16_t)(32 * 1000 / targetPidLooptime);
}
// by default p_ratio is 32 and a P-frame is written every 1ms
// if p_ratio is zero then no P-frames are logged
if (blackboxConfig()->p_ratio == 0) {
blackboxPInterval = 0; // blackboxPInterval not used when p_ratio is zero, so just set it to zero
} else if (blackboxConfig()->p_ratio > blackboxIInterval && blackboxIInterval >= 32) {
blackboxPInterval = 1;
} else {
blackboxPInterval = blackboxIInterval / blackboxConfig()->p_ratio;
}
if (blackboxConfig()->device) {
blackboxSetState(BLACKBOX_STATE_STOPPED);
} else {
blackboxSetState(BLACKBOX_STATE_DISABLED);
}
blackboxSInterval = blackboxIInterval * 256; // S-frame is written every 256*32 = 8192ms, approx every 8 seconds
}
#endif
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