mirror of https://github.com/ArduPilot/ardupilot
468 lines
20 KiB
C++
468 lines
20 KiB
C++
// -*- 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 = 12;
|
|
|
|
// The parameter software_type is set up solely for ground station use
|
|
// and identifies the software type (eg ArduPilotMega versus ArduCopterMega)
|
|
// GCS will interpret values 0-9 as ArduPilotMega. Developers may use
|
|
// values within that range to identify different branches.
|
|
//
|
|
static const uint16_t k_software_type = 0; // 0 for APM trunk
|
|
|
|
//
|
|
// 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,
|
|
k_param_software_type,
|
|
|
|
|
|
// Misc
|
|
//
|
|
|
|
k_param_auto_trim,
|
|
k_param_switch_enable,
|
|
k_param_log_bitmask,
|
|
k_param_pitch_trim,
|
|
k_param_mix_mode,
|
|
k_param_reverse_elevons,
|
|
k_param_reverse_ch1_elevon,
|
|
k_param_reverse_ch2_elevon,
|
|
k_param_flap_1_percent,
|
|
k_param_flap_1_speed,
|
|
k_param_flap_2_percent,
|
|
k_param_flap_2_speed,
|
|
k_param_num_resets,
|
|
k_param_log_last_filenumber,
|
|
|
|
|
|
// 110: Telemetry control
|
|
//
|
|
k_param_streamrates_port0 = 110,
|
|
k_param_streamrates_port3,
|
|
k_param_sysid_this_mav,
|
|
k_param_sysid_my_gcs,
|
|
k_param_serial3_baud,
|
|
|
|
// 120: Fly-by-wire control
|
|
//
|
|
k_param_flybywire_airspeed_min = 120,
|
|
k_param_flybywire_airspeed_max,
|
|
k_param_FBWB_min_altitude, // -1=disabled, minimum value for altitude in cm (default 30m)
|
|
|
|
//
|
|
// 130: Sensor parameters
|
|
//
|
|
k_param_IMU_calibration = 130,
|
|
k_param_altitude_mix,
|
|
k_param_airspeed_ratio,
|
|
k_param_ground_temperature,
|
|
k_param_ground_pressure,
|
|
k_param_compass_enabled,
|
|
k_param_compass,
|
|
k_param_battery_monitoring,
|
|
k_param_volt_div_ratio,
|
|
k_param_curr_amp_per_volt,
|
|
k_param_input_voltage,
|
|
k_param_pack_capacity,
|
|
k_param_airspeed_offset,
|
|
k_param_sonar_enabled,
|
|
k_param_airspeed_enabled,
|
|
|
|
//
|
|
// 150: Navigation parameters
|
|
//
|
|
k_param_crosstrack_gain = 150,
|
|
k_param_crosstrack_entry_angle,
|
|
k_param_roll_limit,
|
|
k_param_pitch_limit_max,
|
|
k_param_pitch_limit_min,
|
|
k_param_airspeed_cruise,
|
|
k_param_RTL_altitude,
|
|
k_param_inverted_flight_ch,
|
|
|
|
//
|
|
// 170: Radio settings
|
|
//
|
|
k_param_channel_roll = 170,
|
|
k_param_channel_pitch,
|
|
k_param_channel_throttle,
|
|
k_param_channel_yaw,
|
|
k_param_rc_5,
|
|
k_param_rc_6,
|
|
k_param_rc_7,
|
|
k_param_rc_8,
|
|
|
|
k_param_throttle_min,
|
|
k_param_throttle_max,
|
|
k_param_throttle_fs_enabled,
|
|
k_param_throttle_fs_value,
|
|
k_param_throttle_cruise,
|
|
|
|
k_param_short_fs_action,
|
|
k_param_long_fs_action,
|
|
k_param_gcs_heartbeat_fs_enabled,
|
|
k_param_throttle_slewrate,
|
|
|
|
//
|
|
// 200: Feed-forward gains
|
|
//
|
|
k_param_kff_pitch_compensation = 200,
|
|
k_param_kff_rudder_mix,
|
|
k_param_kff_pitch_to_throttle,
|
|
k_param_kff_throttle_to_pitch,
|
|
|
|
//
|
|
// 210: flight modes
|
|
//
|
|
k_param_flight_mode_channel = 210,
|
|
k_param_flight_mode1,
|
|
k_param_flight_mode2,
|
|
k_param_flight_mode3,
|
|
k_param_flight_mode4,
|
|
k_param_flight_mode5,
|
|
k_param_flight_mode6,
|
|
|
|
//
|
|
// 220: Waypoint data
|
|
//
|
|
k_param_waypoint_mode = 220,
|
|
k_param_command_total,
|
|
k_param_command_index,
|
|
k_param_waypoint_radius,
|
|
k_param_loiter_radius,
|
|
|
|
//
|
|
// 240: PID Controllers
|
|
//
|
|
// Heading-to-roll PID:
|
|
// heading error from command to roll command deviation from trim
|
|
// (bank to turn strategy)
|
|
//
|
|
k_param_heading_to_roll_PID = 240,
|
|
|
|
// Roll-to-servo PID:
|
|
// roll error from command to roll servo deviation from trim
|
|
// (tracks commanded bank angle)
|
|
//
|
|
k_param_roll_to_servo_PID,
|
|
|
|
//
|
|
// Pitch control
|
|
//
|
|
// Pitch-to-servo PID:
|
|
// pitch error from command to pitch servo deviation from trim
|
|
// (front-side strategy)
|
|
//
|
|
k_param_pitch_to_servo_PID,
|
|
|
|
// Airspeed-to-pitch PID:
|
|
// airspeed error from command to pitch servo deviation from trim
|
|
// (back-side strategy)
|
|
//
|
|
k_param_airspeed_to_pitch_PID,
|
|
|
|
//
|
|
// Yaw control
|
|
//
|
|
// Yaw-to-servo PID:
|
|
// yaw rate error from command to yaw servo deviation from trim
|
|
// (stabilizes dutch roll)
|
|
//
|
|
k_param_yaw_to_servo_PID,
|
|
|
|
//
|
|
// Throttle control
|
|
//
|
|
// Energy-to-throttle PID:
|
|
// total energy error from command to throttle servo deviation from trim
|
|
// (throttle back-side strategy alternative)
|
|
//
|
|
k_param_energy_to_throttle_PID,
|
|
|
|
// Altitude-to-pitch PID:
|
|
// altitude error from command to pitch servo deviation from trim
|
|
// (throttle front-side strategy alternative)
|
|
//
|
|
k_param_altitude_to_pitch_PID,
|
|
|
|
// 254,255: reserved
|
|
};
|
|
|
|
AP_Int16 format_version;
|
|
AP_Int8 software_type;
|
|
|
|
// Telemetry control
|
|
//
|
|
AP_Int16 sysid_this_mav;
|
|
AP_Int16 sysid_my_gcs;
|
|
AP_Int8 serial3_baud;
|
|
|
|
// Feed-forward gains
|
|
//
|
|
AP_Float kff_pitch_compensation;
|
|
AP_Float kff_rudder_mix;
|
|
AP_Float kff_pitch_to_throttle;
|
|
AP_Float kff_throttle_to_pitch;
|
|
|
|
// Crosstrack navigation
|
|
//
|
|
AP_Float crosstrack_gain;
|
|
AP_Int16 crosstrack_entry_angle;
|
|
|
|
// Estimation
|
|
//
|
|
AP_Float altitude_mix;
|
|
AP_Float airspeed_ratio;
|
|
AP_Int16 airspeed_offset;
|
|
|
|
// Waypoints
|
|
//
|
|
AP_Int8 waypoint_mode;
|
|
AP_Int8 command_total;
|
|
AP_Int8 command_index;
|
|
AP_Int8 waypoint_radius;
|
|
AP_Int8 loiter_radius;
|
|
|
|
// Fly-by-wire
|
|
//
|
|
AP_Int8 flybywire_airspeed_min;
|
|
AP_Int8 flybywire_airspeed_max;
|
|
AP_Int16 FBWB_min_altitude;
|
|
|
|
// Throttle
|
|
//
|
|
AP_Int8 throttle_min;
|
|
AP_Int8 throttle_max;
|
|
AP_Int8 throttle_slewrate;
|
|
AP_Int8 throttle_fs_enabled;
|
|
AP_Int16 throttle_fs_value;
|
|
AP_Int8 throttle_cruise;
|
|
|
|
// Failsafe
|
|
AP_Int8 short_fs_action;
|
|
AP_Int8 long_fs_action;
|
|
AP_Int8 gcs_heartbeat_fs_enabled;
|
|
|
|
// Flight modes
|
|
//
|
|
AP_Int8 flight_mode_channel;
|
|
AP_Int8 flight_mode1;
|
|
AP_Int8 flight_mode2;
|
|
AP_Int8 flight_mode3;
|
|
AP_Int8 flight_mode4;
|
|
AP_Int8 flight_mode5;
|
|
AP_Int8 flight_mode6;
|
|
|
|
// Navigational maneuvering limits
|
|
//
|
|
AP_Int16 roll_limit;
|
|
AP_Int16 pitch_limit_max;
|
|
AP_Int16 pitch_limit_min;
|
|
|
|
// Misc
|
|
//
|
|
AP_Int8 auto_trim;
|
|
AP_Int8 switch_enable;
|
|
AP_Int8 mix_mode;
|
|
AP_Int8 reverse_elevons;
|
|
AP_Int8 reverse_ch1_elevon;
|
|
AP_Int8 reverse_ch2_elevon;
|
|
AP_Int16 num_resets;
|
|
AP_Int16 log_bitmask;
|
|
AP_Int16 log_last_filenumber;
|
|
AP_Int16 airspeed_cruise;
|
|
AP_Int16 pitch_trim;
|
|
AP_Int16 RTL_altitude;
|
|
AP_Int16 ground_temperature;
|
|
AP_Int32 ground_pressure;
|
|
AP_Int8 compass_enabled;
|
|
AP_Int16 angle_of_attack;
|
|
AP_Int8 battery_monitoring; // 0=disabled, 1=3 cell lipo, 2=4 cell lipo, 3=total voltage only, 4=total voltage and current
|
|
AP_Float volt_div_ratio;
|
|
AP_Float curr_amp_per_volt;
|
|
AP_Float input_voltage;
|
|
AP_Int16 pack_capacity; // Battery pack capacity less reserve
|
|
AP_Int8 inverted_flight_ch; // 0=disabled, 1-8 is channel for inverted flight trigger
|
|
AP_Int8 sonar_enabled;
|
|
AP_Int8 airspeed_enabled;
|
|
AP_Int8 flap_1_percent;
|
|
AP_Int8 flap_1_speed;
|
|
AP_Int8 flap_2_percent;
|
|
AP_Int8 flap_2_speed;
|
|
|
|
// RC channels
|
|
RC_Channel channel_roll;
|
|
RC_Channel channel_pitch;
|
|
RC_Channel channel_throttle;
|
|
RC_Channel channel_rudder;
|
|
RC_Channel_aux rc_5;
|
|
RC_Channel_aux rc_6;
|
|
RC_Channel_aux rc_7;
|
|
RC_Channel_aux rc_8;
|
|
|
|
// PID controllers
|
|
//
|
|
PID pidNavRoll;
|
|
PID pidServoRoll;
|
|
PID pidServoPitch;
|
|
PID pidNavPitchAirspeed;
|
|
PID pidServoRudder;
|
|
PID pidTeThrottle;
|
|
PID pidNavPitchAltitude;
|
|
|
|
uint8_t junk;
|
|
|
|
// Note: keep initializers here in the same order as they are declared above.
|
|
Parameters() :
|
|
// variable default key name
|
|
//-------------------------------------------------------------------------------------------------------
|
|
format_version (k_format_version, k_param_format_version, PSTR("SYSID_SW_MREV")),
|
|
software_type (k_software_type, k_param_software_type, PSTR("SYSID_SW_TYPE")),
|
|
|
|
sysid_this_mav (MAV_SYSTEM_ID, k_param_sysid_this_mav, PSTR("SYSID_THISMAV")),
|
|
sysid_my_gcs (255, k_param_sysid_my_gcs, PSTR("SYSID_MYGCS")),
|
|
serial3_baud (SERIAL3_BAUD/1000, k_param_serial3_baud, PSTR("SERIAL3_BAUD")),
|
|
|
|
kff_pitch_compensation (PITCH_COMP, k_param_kff_pitch_compensation, PSTR("KFF_PTCHCOMP")),
|
|
kff_rudder_mix (RUDDER_MIX, k_param_kff_rudder_mix, PSTR("KFF_RDDRMIX")),
|
|
kff_pitch_to_throttle (P_TO_T, k_param_kff_pitch_to_throttle, PSTR("KFF_PTCH2THR")),
|
|
kff_throttle_to_pitch (T_TO_P, k_param_kff_throttle_to_pitch, PSTR("KFF_THR2PTCH")),
|
|
|
|
crosstrack_gain (XTRACK_GAIN_SCALED, k_param_crosstrack_gain, PSTR("XTRK_GAIN_SC")),
|
|
crosstrack_entry_angle (XTRACK_ENTRY_ANGLE_CENTIDEGREE,k_param_crosstrack_entry_angle, PSTR("XTRK_ANGLE_CD")),
|
|
|
|
altitude_mix (ALTITUDE_MIX, k_param_altitude_mix, PSTR("ALT_MIX")),
|
|
airspeed_ratio (AIRSPEED_RATIO, k_param_airspeed_ratio, PSTR("ARSPD_RATIO")),
|
|
airspeed_offset (0, k_param_airspeed_offset, PSTR("ARSPD_OFFSET")),
|
|
|
|
/* XXX waypoint_mode missing here */
|
|
command_total (0, k_param_command_total, PSTR("CMD_TOTAL")),
|
|
command_index (0, k_param_command_index, PSTR("CMD_INDEX")),
|
|
waypoint_radius (WP_RADIUS_DEFAULT, k_param_waypoint_radius, PSTR("WP_RADIUS")),
|
|
loiter_radius (LOITER_RADIUS_DEFAULT, k_param_loiter_radius, PSTR("WP_LOITER_RAD")),
|
|
|
|
flybywire_airspeed_min (AIRSPEED_FBW_MIN, k_param_flybywire_airspeed_min, PSTR("ARSPD_FBW_MIN")),
|
|
flybywire_airspeed_max (AIRSPEED_FBW_MAX, k_param_flybywire_airspeed_max, PSTR("ARSPD_FBW_MAX")),
|
|
|
|
throttle_min (THROTTLE_MIN, k_param_throttle_min, PSTR("THR_MIN")),
|
|
throttle_max (THROTTLE_MAX, k_param_throttle_max, PSTR("THR_MAX")),
|
|
throttle_slewrate (THROTTLE_SLEW_LIMIT, k_param_throttle_slewrate, PSTR("THR_SLEWRATE")),
|
|
throttle_fs_enabled (THROTTLE_FAILSAFE, k_param_throttle_fs_enabled, PSTR("THR_FAILSAFE")),
|
|
throttle_fs_value (THROTTLE_FS_VALUE, k_param_throttle_fs_value, PSTR("THR_FS_VALUE")),
|
|
throttle_cruise (THROTTLE_CRUISE, k_param_throttle_cruise, PSTR("TRIM_THROTTLE")),
|
|
|
|
short_fs_action (SHORT_FAILSAFE_ACTION, k_param_short_fs_action, PSTR("FS_SHORT_ACTN")),
|
|
long_fs_action (LONG_FAILSAFE_ACTION, k_param_long_fs_action, PSTR("FS_LONG_ACTN")),
|
|
gcs_heartbeat_fs_enabled(GCS_HEARTBEAT_FAILSAFE, k_param_gcs_heartbeat_fs_enabled, PSTR("FS_GCS_ENABL")),
|
|
|
|
flight_mode_channel (FLIGHT_MODE_CHANNEL, k_param_flight_mode_channel, PSTR("FLTMODE_CH")),
|
|
flight_mode1 (FLIGHT_MODE_1, k_param_flight_mode1, PSTR("FLTMODE1")),
|
|
flight_mode2 (FLIGHT_MODE_2, k_param_flight_mode2, PSTR("FLTMODE2")),
|
|
flight_mode3 (FLIGHT_MODE_3, k_param_flight_mode3, PSTR("FLTMODE3")),
|
|
flight_mode4 (FLIGHT_MODE_4, k_param_flight_mode4, PSTR("FLTMODE4")),
|
|
flight_mode5 (FLIGHT_MODE_5, k_param_flight_mode5, PSTR("FLTMODE5")),
|
|
flight_mode6 (FLIGHT_MODE_6, k_param_flight_mode6, PSTR("FLTMODE6")),
|
|
|
|
roll_limit (HEAD_MAX_CENTIDEGREE, k_param_roll_limit, PSTR("LIM_ROLL_CD")),
|
|
pitch_limit_max (PITCH_MAX_CENTIDEGREE, k_param_pitch_limit_max, PSTR("LIM_PITCH_MAX")),
|
|
pitch_limit_min (PITCH_MIN_CENTIDEGREE, k_param_pitch_limit_min, PSTR("LIM_PITCH_MIN")),
|
|
|
|
auto_trim (AUTO_TRIM, k_param_auto_trim, PSTR("TRIM_AUTO")),
|
|
switch_enable (REVERSE_SWITCH, k_param_switch_enable, PSTR("SWITCH_ENABLE")),
|
|
mix_mode (ELEVON_MIXING, k_param_mix_mode, PSTR("ELEVON_MIXING")),
|
|
reverse_elevons (ELEVON_REVERSE, k_param_reverse_elevons, PSTR("ELEVON_REVERSE")),
|
|
reverse_ch1_elevon (ELEVON_CH1_REVERSE, k_param_reverse_ch1_elevon, PSTR("ELEVON_CH1_REV")),
|
|
reverse_ch2_elevon (ELEVON_CH2_REVERSE, k_param_reverse_ch2_elevon, PSTR("ELEVON_CH2_REV")),
|
|
num_resets (0, k_param_num_resets, PSTR("SYS_NUM_RESETS")),
|
|
log_bitmask (DEFAULT_LOG_BITMASK, k_param_log_bitmask, PSTR("LOG_BITMASK")),
|
|
log_last_filenumber (0, k_param_log_last_filenumber, PSTR("LOG_LASTFILE")),
|
|
airspeed_cruise (AIRSPEED_CRUISE_CM, k_param_airspeed_cruise, PSTR("TRIM_ARSPD_CM")),
|
|
pitch_trim (0, k_param_pitch_trim, PSTR("TRIM_PITCH_CD")),
|
|
RTL_altitude (ALT_HOLD_HOME_CM, k_param_RTL_altitude, PSTR("ALT_HOLD_RTL")),
|
|
FBWB_min_altitude (ALT_HOLD_FBW_CM, k_param_FBWB_min_altitude, PSTR("ALT_HOLD_FBWCM")),
|
|
ground_temperature (0, k_param_ground_temperature, PSTR("GND_TEMP")),
|
|
ground_pressure (0, k_param_ground_pressure, PSTR("GND_ABS_PRESS")),
|
|
compass_enabled (MAGNETOMETER, k_param_compass_enabled, PSTR("MAG_ENABLE")),
|
|
flap_1_percent (FLAP_1_PERCENT, k_param_flap_1_percent, PSTR("FLAP_1_PERCNT")),
|
|
flap_1_speed (FLAP_1_SPEED, k_param_flap_1_speed, PSTR("FLAP_1_SPEED")),
|
|
flap_2_percent (FLAP_2_PERCENT, k_param_flap_2_percent, PSTR("FLAP_2_PERCNT")),
|
|
flap_2_speed (FLAP_2_SPEED, k_param_flap_2_speed, PSTR("FLAP_2_SPEED")),
|
|
|
|
|
|
battery_monitoring (DISABLED, k_param_battery_monitoring, PSTR("BATT_MONITOR")),
|
|
volt_div_ratio (VOLT_DIV_RATIO, k_param_volt_div_ratio, PSTR("VOLT_DIVIDER")),
|
|
curr_amp_per_volt (CURR_AMP_PER_VOLT, k_param_curr_amp_per_volt, PSTR("AMP_PER_VOLT")),
|
|
input_voltage (INPUT_VOLTAGE, k_param_input_voltage, PSTR("INPUT_VOLTS")),
|
|
pack_capacity (HIGH_DISCHARGE, k_param_pack_capacity, PSTR("BATT_CAPACITY")),
|
|
inverted_flight_ch (0, k_param_inverted_flight_ch, PSTR("INVERTEDFLT_CH")),
|
|
sonar_enabled (SONAR_ENABLED, k_param_sonar_enabled, PSTR("SONAR_ENABLE")),
|
|
airspeed_enabled (AIRSPEED_SENSOR, k_param_airspeed_enabled, PSTR("ARSPD_ENABLE")),
|
|
|
|
// Note - total parameter name length must be less than 14 characters for MAVLink compatibility!
|
|
|
|
// RC channel group key name
|
|
//----------------------------------------------------------------------
|
|
channel_roll (k_param_channel_roll, PSTR("RC1_")),
|
|
channel_pitch (k_param_channel_pitch, PSTR("RC2_")),
|
|
channel_throttle (k_param_channel_throttle, PSTR("RC3_")),
|
|
channel_rudder (k_param_channel_yaw, 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_")),
|
|
|
|
// PID controller group key name initial P initial I initial D initial imax
|
|
//---------------------------------------------------------------------------------------------------------------------------------------
|
|
pidNavRoll (k_param_heading_to_roll_PID, PSTR("HDNG2RLL_"), NAV_ROLL_P, NAV_ROLL_I, NAV_ROLL_D, NAV_ROLL_INT_MAX_CENTIDEGREE),
|
|
pidServoRoll (k_param_roll_to_servo_PID, PSTR("RLL2SRV_"), SERVO_ROLL_P, SERVO_ROLL_I, SERVO_ROLL_D, SERVO_ROLL_INT_MAX_CENTIDEGREE),
|
|
pidServoPitch (k_param_pitch_to_servo_PID, PSTR("PTCH2SRV_"), SERVO_PITCH_P, SERVO_PITCH_I, SERVO_PITCH_D, SERVO_PITCH_INT_MAX_CENTIDEGREE),
|
|
pidNavPitchAirspeed (k_param_airspeed_to_pitch_PID, PSTR("ARSP2PTCH_"), NAV_PITCH_ASP_P, NAV_PITCH_ASP_I, NAV_PITCH_ASP_D, NAV_PITCH_ASP_INT_MAX_CMSEC),
|
|
pidServoRudder (k_param_yaw_to_servo_PID, PSTR("YW2SRV_"), SERVO_YAW_P, SERVO_YAW_I, SERVO_YAW_D, SERVO_YAW_INT_MAX),
|
|
pidTeThrottle (k_param_energy_to_throttle_PID, PSTR("ENRGY2THR_"), THROTTLE_TE_P, THROTTLE_TE_I, THROTTLE_TE_D, THROTTLE_TE_INT_MAX),
|
|
pidNavPitchAltitude (k_param_altitude_to_pitch_PID, PSTR("ALT2PTCH_"), NAV_PITCH_ALT_P, NAV_PITCH_ALT_I, NAV_PITCH_ALT_D, NAV_PITCH_ALT_INT_MAX_CM),
|
|
|
|
|
|
junk(0) // XXX just so that we can add things without worrying about the trailing comma
|
|
{
|
|
}
|
|
};
|
|
|
|
#endif // PARAMETERS_H
|