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ardupilot/ArduCopterMega/Parameters.h

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// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
#ifndef PARAMETERS_H
#define PARAMETERS_H
#include <AP_Common.h>
// Global parameter class.
//
class Parameters {
public:
// The version of the layout as described by the parameter enum.
//
// When changing the parameter enum in an incompatible fashion, this
// value should be incremented by one.
//
// The increment will prevent old parameters from being used incorrectly
// by newer code.
//
static const uint16_t k_format_version = 1;
//
// Parameter identities.
//
// The enumeration defined here is used to ensure that every parameter
// or parameter group has a unique ID number. This number is used by
// AP_Var to store and locate parameters in EEPROM.
//
// Note that entries without a number are assigned the next number after
// the entry preceding them. When adding new entries, ensure that they
// don't overlap.
//
// Try to group related variables together, and assign them a set
// range in the enumeration. Place these groups in numerical order
// at the end of the enumeration.
//
// WARNING: Care should be taken when editing this enumeration as the
// AP_Var load/save code depends on the values here to identify
// variables saved in EEPROM.
//
//
enum {
// Layout version number, always key zero.
//
k_param_format_version = 0,
// Misc
//
k_param_log_bitmask,
k_param_frame_type,
//
// 140: Sensor parameters
//
k_param_IMU_calibration = 140,
k_param_ground_temperature,
k_param_ground_altitude,
k_param_ground_pressure,
k_param_current,
k_param_compass,
k_param_mag_declination,
//
// 160: Navigation parameters
//
k_param_crosstrack_gain = 160,
k_param_crosstrack_entry_angle,
k_param_pitch_max,
k_param_RTL_altitude,
//
// 180: Radio settings
//
k_param_rc_1 = 180,
k_param_rc_2,
k_param_rc_3,
k_param_rc_4,
k_param_rc_5,
k_param_rc_6,
k_param_rc_7,
k_param_rc_8,
k_param_rc_9,
k_param_rc_10,
k_param_throttle_min,
k_param_throttle_max,
k_param_throttle_failsafe_enabled,
k_param_throttle_failsafe_action,
k_param_throttle_failsafe_value,
k_param_throttle_cruise,
k_param_flight_mode_channel,
k_param_flight_modes,
//
// 220: Waypoint data
//
k_param_waypoint_mode = 220,
k_param_waypoint_total,
k_param_waypoint_index,
k_param_waypoint_radius,
k_param_loiter_radius,
//
// 240: PID Controllers
//
// Heading-to-roll PID:
// heading error from commnd to roll command deviation from trim
// (bank to turn strategy)
//
k_param_pid_acro_rate_roll = 240,
k_param_pid_acro_rate_pitch,
k_param_pid_acro_rate_yaw,
k_param_pid_stabilize_roll,
k_param_pid_stabilize_pitch,
k_param_pid_yaw,
k_param_pid_nav_lat,
k_param_pid_nav_lon,
k_param_pid_baro_throttle,
k_param_pid_sonar_throttle,
// special D term alternatives
k_param_stabilize_dampener,
k_param_hold_yaw_dampener,
// 255: reserved
};
AP_Int16 format_version;
// Crosstrack navigation
//
AP_Float crosstrack_gain;
AP_Int16 crosstrack_entry_angle;
// Waypoints
//
AP_Int8 waypoint_mode;
AP_Int8 waypoint_total;
AP_Int8 waypoint_index;
AP_Int8 waypoint_radius;
AP_Int8 loiter_radius;
// Throttle
//
AP_Int8 throttle_min;
AP_Int8 throttle_max;
AP_Int8 throttle_failsafe_enabled;
AP_Int8 throttle_failsafe_action;
AP_Int16 throttle_failsafe_value;
AP_Int8 throttle_cruise;
// Flight modes
//
AP_Int8 flight_mode_channel;
AP_VarA<uint8_t,6> flight_modes;
// Radio settings
//
//AP_Var_group pwm_roll;
//AP_Var_group pwm_pitch;
//AP_Var_group pwm_throttle;
//AP_Var_group pwm_yaw;
AP_Int16 pitch_max;
// Misc
//
AP_Int16 log_bitmask;
AP_Int16 ground_temperature;
AP_Int16 ground_altitude;
AP_Int16 ground_pressure;
AP_Int16 RTL_altitude;
AP_Int8 frame_type;
AP_Int8 current_enabled;
AP_Int8 compass_enabled;
AP_Float mag_declination;
// RC channels
RC_Channel rc_1;
RC_Channel rc_2;
RC_Channel rc_3;
RC_Channel rc_4;
RC_Channel rc_5;
RC_Channel rc_6;
RC_Channel rc_7;
RC_Channel rc_8;
RC_Channel rc_camera_pitch;
RC_Channel rc_camera_roll;
// PID controllers
PID pid_acro_rate_roll;
PID pid_acro_rate_pitch;
PID pid_acro_rate_yaw;
PID pid_stabilize_roll;
PID pid_stabilize_pitch;
PID pid_yaw;
PID pid_nav_lat;
PID pid_nav_lon;
PID pid_baro_throttle;
PID pid_sonar_throttle;
AP_Float stabilize_dampener;
AP_Float hold_yaw_dampener;
uint8_t junk;
Parameters() :
// variable default key name
//-------------------------------------------------------------------------------------------------------
format_version (k_format_version, k_param_format_version, NULL),
crosstrack_gain (XTRACK_GAIN_SCALED, k_param_crosstrack_gain, PSTR("XTRK_GAIN_SCALED")),
crosstrack_entry_angle (XTRACK_ENTRY_ANGLE_CENTIDEGREE,k_param_crosstrack_entry_angle, PSTR("XTRACK_ENTRY_ANGLE_CENTIDEGREE")),
frame_type (FRAME_CONFIG, k_param_frame_type, PSTR("FRAME_CONFIG")),
current_enabled (DISABLED, k_param_current, PSTR("CURRENT_ENABLE")),
compass_enabled (DISABLED, k_param_compass, PSTR("COMPASS_ENABLE")),
mag_declination (0, k_param_mag_declination, PSTR("MAG_DEC")),
waypoint_mode (0, k_param_waypoint_mode, PSTR("WP_MODE")),
waypoint_total (0, k_param_waypoint_total, PSTR("WP_TOTAL")),
waypoint_index (0, k_param_waypoint_index, PSTR("WP_INDEX")),
waypoint_radius (WP_RADIUS_DEFAULT, k_param_waypoint_radius, PSTR("WP_RADIUS")),
loiter_radius (LOITER_RADIUS_DEFAULT, k_param_loiter_radius, PSTR("LOITER_RADIUS")),
throttle_min (THROTTLE_MIN, k_param_throttle_min, PSTR("THR_MIN")),
throttle_max (THROTTLE_MAX, k_param_throttle_max, PSTR("THR_MAX")),
throttle_failsafe_enabled (THROTTLE_FAILSAFE, k_param_throttle_failsafe_enabled, PSTR("THR_FAILSAFE")),
throttle_failsafe_action (THROTTLE_FAILSAFE_ACTION, k_param_throttle_failsafe_action, PSTR("THR_FS_ACTION")),
throttle_failsafe_value (THROTTLE_FS_VALUE, k_param_throttle_failsafe_value, PSTR("THR_FS_VALUE")),
throttle_cruise (THROTTLE_CRUISE, k_param_throttle_cruise, PSTR("TRIM_THROTTLE")),
flight_mode_channel (FLIGHT_MODE_CHANNEL, k_param_flight_mode_channel, PSTR("FLIGHT_MODE_CH")),
flight_modes (k_param_flight_modes, PSTR("FLIGHT_MODES")),
pitch_max (PITCH_MAX_CENTIDEGREE, k_param_pitch_max, PSTR("PITCH_MAX_CENTIDEGREE")),
log_bitmask (0, k_param_log_bitmask, PSTR("LOG_BITMASK")),
ground_temperature (0, k_param_ground_temperature, PSTR("GND_TEMP")),
ground_altitude (0, k_param_ground_altitude, PSTR("GND_ALT_CM")),
ground_pressure (0, k_param_ground_pressure, PSTR("GND_ABS_PRESS")),
RTL_altitude (ALT_HOLD_HOME_CM, k_param_RTL_altitude, PSTR("ALT_HOLD_RTL")),
// RC channel group key name
//----------------------------------------------------------------------
rc_1 (k_param_rc_1, PSTR("RC1_")),
rc_2 (k_param_rc_2, PSTR("RC2_")),
rc_3 (k_param_rc_3, PSTR("RC3_")),
rc_4 (k_param_rc_4, PSTR("RC4_")),
rc_5 (k_param_rc_5, PSTR("RC5_")),
rc_6 (k_param_rc_6, PSTR("RC6_")),
rc_7 (k_param_rc_7, PSTR("RC7_")),
rc_8 (k_param_rc_8, PSTR("RC8_")),
rc_camera_pitch (k_param_rc_8, PSTR("RC9_")),
rc_camera_roll (k_param_rc_8, PSTR("RC10_")),
// PID controller group key name initial P initial I initial D initial imax
//---------------------------------------------------------------------------------------------------------------------------------------
pid_acro_rate_roll (k_param_pid_acro_rate_roll, PSTR("ACR_RLL_"), ACRO_RATE_ROLL_P, ACRO_RATE_ROLL_I, ACRO_RATE_ROLL_D, ACRO_RATE_ROLL_IMAX_CENTIDEGREE),
pid_acro_rate_pitch (k_param_pid_acro_rate_pitch, PSTR("ACR_PIT_"), ACRO_RATE_PITCH_P, ACRO_RATE_PITCH_I, ACRO_RATE_PITCH_D, ACRO_RATE_PITCH_IMAX_CENTIDEGREE),
pid_acro_rate_yaw (k_param_pid_acro_rate_yaw, PSTR("ACR_YAW_"), ACRO_RATE_YAW_P, ACRO_RATE_YAW_I, ACRO_RATE_YAW_D, ACRO_RATE_YAW_IMAX_CENTIDEGREE),
pid_stabilize_roll (k_param_pid_stabilize_roll, PSTR("STB_RLL_"), STABILIZE_ROLL_P, STABILIZE_ROLL_I, STABILIZE_ROLL_D, STABILIZE_ROLL_IMAX_CENTIDEGREE),
pid_stabilize_pitch (k_param_pid_stabilize_pitch, PSTR("STB_PIT_"), STABILIZE_PITCH_P, STABILIZE_PITCH_I, STABILIZE_PITCH_D, STABILIZE_PITCH_IMAX_CENTIDEGREE),
pid_yaw (k_param_pid_yaw, PSTR("STB_YAW_"), YAW_P, YAW_I, YAW_D, YAW_IMAX_CENTIDEGREE),
pid_nav_lat (k_param_pid_nav_lat, PSTR("NAV_LAT_"), NAV_P, NAV_I, NAV_D, NAV_IMAX_CENTIDEGREE),
pid_nav_lon (k_param_pid_nav_lon, PSTR("NAV_LON_"), NAV_P, NAV_I, NAV_D, NAV_IMAX_CENTIDEGREE),
pid_baro_throttle (k_param_pid_baro_throttle, PSTR("THR_BAR_"), THROTTLE_BARO_P, THROTTLE_BARO_I, THROTTLE_BARO_D, THROTTLE_BARO_IMAX_CENTIDEGREE),
pid_sonar_throttle (k_param_pid_sonar_throttle, PSTR("THR_SON_"), THROTTLE_SONAR_P, THROTTLE_SONAR_I, THROTTLE_SONAR_D, THROTTLE_SONAR_IMAX_CENTIDEGREE),
stabilize_dampener (STABILIZE_DAMPENER, k_param_stabilize_dampener, PSTR("STB_DAMP")),
hold_yaw_dampener (HOLD_YAW_DAMPENER, k_param_hold_yaw_dampener, PSTR("YAW_DAMP")),
junk(0) // XXX just so that we can add things without worrying about the trailing comma
{
}
};
#endif // PARAMETERS_H
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