// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: t -*- // ************************************************************************************ // This function gets critical data from EEPROM to get us underway if restarting in air // ************************************************************************************ // Macro functions // --------------- void read_EEPROM_startup(void) { read_EEPROM_PID(); read_EEPROM_frame(); read_EEPROM_configs(); read_EEPROM_flight_modes(); read_EEPROM_waypoint_info(); imu.load_gyro_eeprom(); imu.load_accel_eeprom(); read_EEPROM_alt_RTL(); // magnatometer read_EEPROM_mag(); read_EEPROM_mag_declination(); read_EEPROM_mag_offset(); } void read_EEPROM_airstart_critical(void) { int16_t temp = 0; imu.load_gyro_eeprom(); imu.load_accel_eeprom(); // Read the home location //----------------------- home = get_wp_with_index(0); // Read pressure sensor values //---------------------------- read_EEPROM_pressure(); } void save_EEPROM_groundstart(void) { rc_1.save_trim(); rc_2.save_trim(); rc_3.save_trim(); rc_4.save_trim(); rc_5.save_trim(); rc_6.save_trim(); rc_7.save_trim(); rc_8.save_trim(); // pressure sensor data saved by init_home } /********************************************************************************/ long read_alt_to_hold() { read_EEPROM_alt_RTL(); if(alt_to_hold == -1) return current_loc.alt; else return alt_to_hold + home.alt; } /********************************************************************************/ void save_EEPROM_alt_RTL(void) { eeprom_write_dword((uint32_t *)EE_ALT_HOLD_HOME, alt_to_hold); } void read_EEPROM_alt_RTL(void) { alt_to_hold = eeprom_read_dword((const uint32_t *) EE_ALT_HOLD_HOME); } /********************************************************************************/ void read_EEPROM_waypoint_info(void) { wp_total = eeprom_read_byte((uint8_t *) EE_WP_TOTAL); wp_radius = eeprom_read_byte((uint8_t *) EE_WP_RADIUS); loiter_radius = eeprom_read_byte((uint8_t *) EE_LOITER_RADIUS); } void save_EEPROM_waypoint_info(void) { eeprom_write_byte((uint8_t *) EE_WP_TOTAL, wp_total); eeprom_write_byte((uint8_t *) EE_WP_RADIUS, wp_radius); eeprom_write_byte((uint8_t *) EE_LOITER_RADIUS, loiter_radius); } /********************************************************************************/ void read_EEPROM_nav(void) { // for nav estimation distance_gain = read_EE_compressed_float(EE_DISTANCE_GAIN, 4); altitude_gain = read_EE_compressed_float(EE_ALTITUDE_GAIN, 4); // stored as degree * 100 x_track_gain = read_EE_compressed_float(EE_XTRACK_GAIN, 4); x_track_angle = eeprom_read_word((uint16_t *) EE_XTRACK_ANGLE) * 100; pitch_max = eeprom_read_word((uint16_t *) EE_PITCH_MAX); // scale to degress * 100 } void save_EEPROM_nav(void) { // for nav estimation write_EE_compressed_float(altitude_gain, EE_ALTITUDE_GAIN, 4); write_EE_compressed_float(distance_gain, EE_DISTANCE_GAIN, 4); write_EE_compressed_float(x_track_gain, EE_XTRACK_GAIN, 4); // stored as degrees eeprom_write_word((uint16_t *) EE_XTRACK_ANGLE, x_track_angle / 100); // stored as degrees eeprom_write_word((uint16_t *) EE_PITCH_MAX, pitch_max); } /********************************************************************************/ void read_EEPROM_PID(void) { pid_acro_rate_roll.load_gains(); pid_acro_rate_pitch.load_gains(); pid_acro_rate_yaw.load_gains(); pid_stabilize_roll.load_gains(); pid_stabilize_pitch.load_gains(); pid_yaw.load_gains(); pid_nav.load_gains(); pid_throttle.load_gains(); // roll pitch stabilize_dampener = read_EE_compressed_float(EE_STAB_DAMPENER, 4); // yaw hold_yaw_dampener = read_EE_compressed_float(EE_HOLD_YAW_DAMPENER, 4); } void save_EEPROM_PID(void) { pid_acro_rate_roll.save_gains(); pid_acro_rate_pitch.save_gains(); pid_acro_rate_yaw.save_gains(); pid_stabilize_roll.save_gains(); pid_stabilize_pitch.save_gains(); pid_yaw.save_gains(); pid_nav.save_gains(); pid_throttle.save_gains(); // roll pitch write_EE_compressed_float(stabilize_dampener, EE_STAB_DAMPENER, 4); // yaw write_EE_compressed_float(hold_yaw_dampener, EE_HOLD_YAW_DAMPENER, 4); } /********************************************************************************/ void save_EEPROM_frame(void) { eeprom_write_byte((uint8_t *)EE_FRAME, frame_type); } void read_EEPROM_frame(void) { frame_type = eeprom_read_byte((uint8_t *) EE_FRAME); } /********************************************************************************/ void save_EEPROM_throttle_cruise(void) { eeprom_write_word((uint16_t *)EE_THROTTLE_CRUISE, throttle_cruise); } void read_EEPROM_throttle_cruise(void) { throttle_cruise = eeprom_read_word((uint16_t *) EE_THROTTLE_CRUISE); } /********************************************************************************/ void save_EEPROM_mag_declination(void) { write_EE_compressed_float(mag_declination, EE_MAG_DECLINATION, 1); } void read_EEPROM_mag_declination(void) { mag_declination = read_EE_compressed_float(EE_MAG_DECLINATION, 1); } /********************************************************************************/ void save_EEPROM_mag_offset(void) { write_EE_compressed_float(mag_offset_x, EE_MAG_X, 2); write_EE_compressed_float(mag_offset_y, EE_MAG_Y, 2); write_EE_compressed_float(mag_offset_z, EE_MAG_Z, 2); } void read_EEPROM_mag_offset(void) { mag_offset_x = read_EE_compressed_float(EE_MAG_X, 2); mag_offset_y = read_EE_compressed_float(EE_MAG_Y, 2); mag_offset_z = read_EE_compressed_float(EE_MAG_Z, 2); } /********************************************************************************/ void read_EEPROM_mag(void) { compass_enabled = eeprom_read_byte((uint8_t *) EE_COMPASS); } void save_EEPROM_mag(void) { eeprom_write_byte((uint8_t *) EE_COMPASS, compass_enabled); } /********************************************************************************/ void save_command_index(void) { eeprom_write_byte((uint8_t *) EE_WP_INDEX, command_must_index); } void read_command_index(void) { wp_index = command_must_index = eeprom_read_byte((uint8_t *) EE_WP_INDEX); } /********************************************************************************/ void save_EEPROM_pressure(void) { eeprom_write_dword((uint32_t *)EE_ABS_PRESS_GND, abs_pressure_ground); eeprom_write_word((uint16_t *)EE_GND_TEMP, ground_temperature); } void read_EEPROM_pressure(void) { abs_pressure_ground = eeprom_read_dword((uint32_t *) EE_ABS_PRESS_GND); // Better than zero for an air start value abs_pressure = abs_pressure_ground; ground_temperature = eeprom_read_word((uint16_t *) EE_GND_TEMP); } /********************************************************************************/ void read_EEPROM_radio(void) { rc_1.load_eeprom(); rc_2.load_eeprom(); rc_3.load_eeprom(); rc_4.load_eeprom(); rc_5.load_eeprom(); rc_6.load_eeprom(); rc_7.load_eeprom(); rc_8.load_eeprom(); } void save_EEPROM_radio(void) { rc_1.save_eeprom(); rc_2.save_eeprom(); rc_3.save_eeprom(); rc_4.save_eeprom(); rc_5.save_eeprom(); rc_6.save_eeprom(); rc_7.save_eeprom(); rc_8.save_eeprom(); } /********************************************************************************/ // configs are the basics void read_EEPROM_configs(void) { throttle_min = eeprom_read_word((uint16_t *) EE_THROTTLE_MIN); throttle_max = eeprom_read_word((uint16_t *) EE_THROTTLE_MAX); read_EEPROM_throttle_cruise(); throttle_failsafe_enabled = eeprom_read_byte((byte *) EE_THROTTLE_FAILSAFE); throttle_failsafe_action = eeprom_read_byte((byte *) EE_THROTTLE_FAILSAFE_ACTION); throttle_failsafe_value = eeprom_read_word((uint16_t *) EE_THROTTLE_FS_VALUE); log_bitmask = eeprom_read_word((uint16_t *) EE_LOG_BITMASK); } void save_EEPROM_configs(void) { eeprom_write_word((uint16_t *) EE_THROTTLE_MIN, throttle_min); eeprom_write_word((uint16_t *) EE_THROTTLE_MAX, throttle_max); save_EEPROM_throttle_cruise(); eeprom_write_byte((byte *) EE_THROTTLE_FAILSAFE, throttle_failsafe_enabled); eeprom_write_byte((byte *) EE_THROTTLE_FAILSAFE_ACTION,throttle_failsafe_action); eeprom_write_word((uint16_t *) EE_THROTTLE_FS_VALUE, throttle_failsafe_value); eeprom_write_word((uint16_t *) EE_LOG_BITMASK, log_bitmask); } /********************************************************************************/ void read_EEPROM_flight_modes(void) { // Read Radio min/max settings eeprom_read_block((void*)&flight_modes, (const void*)EE_FLIGHT_MODES, sizeof(flight_modes)); } void save_EEPROM_flight_modes(void) { // Save Radio min/max settings eeprom_write_block((const void *)&flight_modes, (void *)EE_FLIGHT_MODES, sizeof(flight_modes)); } /********************************************************************************/ float read_EE_float(int address) { union { byte bytes[4]; float value; } _floatOut; for (int i = 0; i < 4; i++) _floatOut.bytes[i] = eeprom_read_byte((uint8_t *) (address + i)); return _floatOut.value; } void write_EE_float(float value, int address) { union { byte bytes[4]; float value; } _floatIn; _floatIn.value = value; for (int i = 0; i < 4; i++) eeprom_write_byte((uint8_t *) (address + i), _floatIn.bytes[i]); } /********************************************************************************/ float read_EE_compressed_float(int address, byte places) { float scale = pow(10, places); int temp = eeprom_read_word((uint16_t *) address); return ((float)temp / scale); } void write_EE_compressed_float(float value, int address, byte places) { float scale = pow(10, places); int temp = value * scale; eeprom_write_word((uint16_t *) address, temp); }