mirror of https://github.com/ArduPilot/ardupilot
cleaning up code and adding functions from APM main code
git-svn-id: https://arducopter.googlecode.com/svn/trunk@250 f9c3cf11-9bcb-44bc-f272-b75c42450872
This commit is contained in:
jphelirc
parent
12d54e7e72
commit
36628eeb06
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@ -27,6 +27,12 @@
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// User configurable settings are on UserConfig.h
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/*******************************************************************/
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/**************************************************************/
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// Special features that might disapear in future releases
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//#define jpframe // This is only Jani's special frame, you should never use unless you know what you are doing
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// As default this should be always checked off.
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/* APM Hardware definitions */
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#define LED_Yellow 36
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@ -48,12 +54,16 @@
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uint8_t sensors[6] = {1, 2, 0, 4, 5, 6}; // For ArduPilot Mega Sensor Shield Hardware
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// Sensor: GYROX, GYROY, GYROZ, ACCELX, ACCELY, ACCELZ, MAGX, MAGY, MAGZ
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int SENSOR_SIGN[]={
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1, -1, -1, // GYROX, GYROY, GYROZ
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-1, 1, 1, // ACCELX, ACCELY, ACCELZ
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-1, -1, -1}; // MAGNETOX, MAGNETOY, MAGNETOZ
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//{-1,1,-1,1,-1,1,-1,-1,-1};
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#ifndef jpframe
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int SENSOR_SIGN[]={
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1, -1, -1, -1, 1, 1, -1, -1, -1};
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//{-1,1,-1,1,-1,1,-1,-1,-1};
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#else
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int SENSOR_SIGN[]={
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1, -1, 1, -1, 1, 1, -1, -1, -1};
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//{-1,1,-1,1,-1,1,-1,-1,-1};
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#endif
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/* APM Hardware definitions, END */
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@ -94,51 +104,39 @@ int gyro_temp;
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float G_Dt=0.02; // Integration time for the gyros (DCM algorithm)
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float Accel_Vector[3]= {0, 0, 0}; //Store the acceleration in a vector
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float Accel_Vector_unfiltered[3]= {0, 0, 0}; //Store the acceleration in a vector
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float Gyro_Vector[3]= {0, 0, 0};//Store the gyros rutn rate in a vector
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float Gyro_Vector[3]= {0, 0, 0}; //Store the gyros rutn rate in a vector
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float Omega_Vector[3]= {0, 0, 0}; //Corrected Gyro_Vector data
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float Omega_P[3]= {0, 0, 0};//Omega Proportional correction
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float Omega_I[3]= {0, 0, 0};//Omega Integrator
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float Omega_P[3]= {0, 0, 0}; //Omega Proportional correction
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float Omega_I[3]= {0, 0, 0}; //Omega Integrator
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float Omega[3]= {0, 0, 0};
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//float Accel_magnitude;
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//float Accel_weight;
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float errorRollPitch[3]= {0, 0, 0};
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float errorYaw[3]= {0, 0, 0};
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float errorCourse=0;
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float COGX=0; //Course overground X axis
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float COGY=1; //Course overground Y axis
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float errorRollPitch[3] = {0, 0, 0};
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float errorYaw[3] = {0, 0, 0};
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float errorCourse = 0;
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float COGX = 0; //Course overground X axis
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float COGY = 1; //Course overground Y axis
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float roll=0;
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float pitch=0;
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float yaw=0;
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float roll = 0;
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float pitch = 0;
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float yaw = 0;
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unsigned int counter=0;
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unsigned int counter = 0;
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float DCM_Matrix[3][3]= {
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{
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1,0,0 }
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,{
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0,1,0 }
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,{
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0,0,1 }
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};
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{ 1,0,0 },
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{ 0,1,0 },
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{ 0,0,1 }};
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float Update_Matrix[3][3]={
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{
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0,1,2 }
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,{
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3,4,5 }
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,{
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6,7,8 }
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}; //Gyros here
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{ 0,1,2 },
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{ 3,4,5 },
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{ 6,7,8 }}; //Gyros here
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float Temporary_Matrix[3][3]={
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{
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0,0,0 }
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,{
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0,0,0 }
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,{
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0,0,0 }
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};
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{ 0,0,0 },
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{ 0,0,0 },
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{ 0,0,0 }};
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// GPS variables
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float speed_3d=0;
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@ -200,6 +198,30 @@ float command_altitude;
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float altitude_I;
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float altitude_D;
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//Pressure Sensor variables
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#ifdef UseBMP
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unsigned long abs_press = 0;
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unsigned long abs_press_filt = 0;
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unsigned long abs_press_gnd = 0;
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int ground_temperature = 0; //
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int temp_unfilt = 0;
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long ground_alt = 0; // Ground altitude from gps at startup in centimeters
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long press_alt = 0; // Pressure altitude
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#endif
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#define BATTERY_VOLTAGE(x) (x*(INPUT_VOLTAGE/1024.0))*VOLT_DIV_RATIO
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#define AIRSPEED_PIN 1 // Need to correct value
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#define BATTERY_PIN 1 // Need to correct value
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#define RELAY_PIN 47
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#define LOW_VOLTAGE 11.4 // Pack voltage at which to trigger alarm
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#define INPUT_VOLTAGE 5.2 // (Volts) voltage your power regulator is feeding your ArduPilot to have an accurate pressure and battery level readings. (you need a multimeter to measure and set this of course)
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#define VOLT_DIV_RATIO 1.0 // Voltage divider ratio set with thru-hole resistor (see manual)
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float battery_voltage = LOW_VOLTAGE * 1.05; // Battery Voltage, initialized above threshold for filter
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// Sonar variables
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int Sonar_value=0;
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#define SonarToCm(x) (x*1.26) // Sonar raw value to centimeters
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@ -30,6 +30,11 @@
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GEAR OFF = Flight Assist (Stable Mode)
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**** LED Feedback ****
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Bootup Sequence:
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1) A, B, C LED's blinking rapidly while waiting ESCs to bootup and initial shake to end from connecting battery
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2) A, B, C LED's have running light while calibrating Gyro/Acc's
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3) Green LED Solid after initialization finished
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Green LED On = APM Initialization Finished
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Yellow LED On = GPS Hold Mode
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Yellow LED Off = Flight Assist Mode (No GPS)
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@ -38,6 +43,7 @@
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Green LED blink slow = Motors armed, Stable mode
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Green LED blink rapid = Motors armed, Acro mode
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*/
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/* User definable modules */
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@ -51,6 +57,18 @@
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#define CONFIGURATOR // Do se use Configurator or normal text output over serial link
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/**********************************************/
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// Not in use yet, starting to work with battery monitors and pressure sensors.
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// Added 19-08-2010
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//#define UseAirspeed
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//#define UseBMP
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//#define BATTERY_EVENT 1 // (boolean) 0 = don't read battery, 1 = read battery voltage (only if you have it wired up!)
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/**********************************************/
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/* User definable modules - END */
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// Frame build condiguration
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@ -67,6 +85,9 @@
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#include <APM_RC.h>
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#include <DataFlash.h>
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#include <APM_Compass.h>
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#ifdef UseBMP
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#include <APM_BMP085.h>
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#endif
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//#include <GPS_NMEA.h> // General NMEA GPS
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#include <GPS_MTK.h> // MediaTEK DIY Drones GPS.
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@ -77,7 +98,8 @@
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#include "ArduCopter.h"
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#include "UserConfig.h"
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#define SWVER 1.31 // Current software version (only numeric values)
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/* Software version */
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#define VER 1.32 // Current software version (only numeric values)
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/* ***************************************************************************** */
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@ -85,7 +107,7 @@
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/* ***************************************************************************** */
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// Normal users does not need to edit anything below these lines. If you have
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// need, go and change them in FrameConfig.h
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// need, go and change them in UserConfig.h
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/* ************************************************************ */
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// STABLE MODE
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@ -127,14 +149,14 @@ void Attitude_control_v2()
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else
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err_pitch = (command_rx_pitch + command_gps_pitch) - ToDeg(pitch); // Position Control
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err_pitch = constrain(err_pitch,-25,25); // to limit max pitch command...
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err_pitch = constrain(err_pitch, -25, 25); // to limit max pitch command...
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// New control term...
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pitch_rate = ToDeg(Omega[1]);
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err_pitch_rate = ((ch_pitch - pitch_mid) >> 1) - pitch_rate;
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pitch_I += err_pitch*G_Dt;
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pitch_I = constrain(pitch_I,-20,20);
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pitch_I += err_pitch * G_Dt;
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pitch_I = constrain(pitch_I, -20, 20);
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// D term
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pitch_D = - pitch_rate;
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@ -197,7 +219,7 @@ void Rate_control()
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err_yaw = ((ch_yaw - yaw_mid) * xmitFactor) - currentYawRate;
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yaw_I += err_yaw*G_Dt;
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yaw_I = constrain(yaw_I,-20,20);
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yaw_I = constrain(yaw_I, -20, 20);
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yaw_D = currentYawRate - previousYawRate;
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previousYawRate = currentYawRate;
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@ -215,15 +237,15 @@ int channel_filter(int ch, int ch_old)
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if (ch_old==0) // ch_old not initialized
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return(ch);
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diff_ch_old = ch - ch_old; // Difference with old reading
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if (diff_ch_old<0)
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if (diff_ch_old < 0)
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{
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if (diff_ch_old<-40)
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return(ch_old-40); // We limit the max difference between readings
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if (diff_ch_old <- 40)
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return(ch_old - 40); // We limit the max difference between readings
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}
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else
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{
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if (diff_ch_old>40)
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return(ch_old+40);
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if (diff_ch_old > 40)
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return(ch_old + 40);
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}
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return((ch + ch_old) >> 1); // Small filtering
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//return(ch);
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@ -234,7 +256,7 @@ int channel_filter(int ch, int ch_old)
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/* ************************************************************ */
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void setup()
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{
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int i;
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int i, j;
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float aux_float[3];
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pinMode(LED_Yellow,OUTPUT); //Yellow LED A (PC1)
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@ -246,7 +268,17 @@ void setup()
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pinMode(RELE_pin,OUTPUT); // Rele output
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digitalWrite(RELE_pin,LOW);
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delay(1000); // Wait until frame is not moving after initial power cord has connected
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// delay(1000); // Wait until frame is not moving after initial power cord has connected
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for(i = 0; i <= 50; i++) {
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digitalWrite(LED_Green, HIGH);
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digitalWrite(LED_Yellow, HIGH);
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digitalWrite(LED_Red, HIGH);
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delay(20);
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digitalWrite(LED_Green, LOW);
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digitalWrite(LED_Yellow, LOW);
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digitalWrite(LED_Red, LOW);
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delay(20);
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}
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APM_RC.Init(); // APM Radio initialization
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APM_ADC.Init(); // APM ADC library initialization
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@ -269,7 +301,6 @@ void setup()
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if(pitch_mid < 1400 || pitch_mid > 1600) pitch_mid = 1500;
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if(yaw_mid < 1400 || yaw_mid > 1600) yaw_mid = 1500;
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// RC channels Initialization (Quad motors)
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APM_RC.OutputCh(0,MIN_THROTTLE); // Motors stoped
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APM_RC.OutputCh(1,MIN_THROTTLE);
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@ -306,6 +337,7 @@ void setup()
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aux_float[1] = gyro_offset_pitch;
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aux_float[2] = gyro_offset_yaw;
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j = 0;
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// Take the gyro offset values
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for(i=0;i<300;i++)
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{
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@ -319,20 +351,42 @@ void setup()
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//Serial.println();
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Log_Write_Sensor(AN[0],AN[1],AN[2],AN[3],AN[4],AN[5],ch_throttle);
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delay(10);
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// Runnings lights effect to let user know that we are taking mesurements
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if(j == 0) {
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digitalWrite(LED_Green, HIGH);
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digitalWrite(LED_Yellow, LOW);
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digitalWrite(LED_Red, LOW);
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}
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else if (j == 1) {
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digitalWrite(LED_Green, LOW);
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digitalWrite(LED_Yellow, HIGH);
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digitalWrite(LED_Red, LOW);
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}
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else {
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digitalWrite(LED_Green, LOW);
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digitalWrite(LED_Yellow, LOW);
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digitalWrite(LED_Red, HIGH);
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}
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if((i % 5) == 0) j++;
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if(j >= 3) j = 0;
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}
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digitalWrite(LED_Green, LOW);
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digitalWrite(LED_Yellow, LOW);
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digitalWrite(LED_Red, LOW);
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for(int y=0; y<=2; y++)
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AN_OFFSET[y]=aux_float[y];
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// Neutro_yaw = APM_RC.InputCh(3); // Take yaw neutral radio value
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// Neutro_yaw = APM_RC.InputCh(3); // Take yaw neutral radio value
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#ifndef CONFIGURATOR
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for(i=0;i<6;i++)
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{
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Serial.print("AN[]:");
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Serial.println(AN_OFFSET[i]);
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}
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Serial.print("Yaw neutral value:");
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// Serial.println(Neutro_yaw);
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// Serial.println(Neutro_yaw);
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Serial.print(yaw_mid);
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#endif
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@ -367,9 +421,11 @@ void setup()
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Read_adc_raw(); // Initialize ADC readings...
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delay(20);
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#ifdef IsAM
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// Switch Left & Right lights on
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digitalWrite(RI_LED, HIGH);
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digitalWrite(LE_LED, HIGH);
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#endif
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motorArmed = 0;
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digitalWrite(LED_Green,HIGH); // Ready to go...
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@ -384,12 +440,12 @@ void loop(){
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int aux;
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int i;
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float aux_float;
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//Log variables
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int log_roll;
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int log_pitch;
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int log_yaw;
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if((millis()-timer)>=10) // Main loop 100Hz
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{
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counter++;
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@ -409,12 +465,13 @@ void loop(){
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}
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}
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#endif
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Matrix_update();
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Normalize();
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Drift_correction();
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Euler_angles();
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// *****************
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// *****************
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// Output data
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log_roll = ToDeg(roll) * 10;
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log_pitch = ToDeg(pitch) * 10;
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@ -427,7 +484,7 @@ void loop(){
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Serial.print(",");
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Serial.print(log_yaw);
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for (int i=0;i<6;i++)
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for (int i = 0; i < 6; i++)
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{
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Serial.print(AN[i]);
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Serial.print(",");
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@ -439,7 +496,7 @@ void loop(){
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// Write attitude to DataFlash log
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Log_Write_Attitude(log_roll,log_pitch,log_yaw);
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if (APM_RC.GetState()==1) // New radio frame?
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if (APM_RC.GetState() == 1) // New radio frame?
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{
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// Commands from radio Rx...
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// Stick position defines the desired angle in roll, pitch and yaw
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@ -455,7 +512,7 @@ void loop(){
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command_rx_pitch_old = command_rx_pitch;
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command_rx_pitch = (ch_pitch-CHANN_CENTER) / 12.0;
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command_rx_pitch_diff = command_rx_pitch - command_rx_pitch_old;
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// aux_float = (ch_yaw-Neutro_yaw) / 180.0;
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// aux_float = (ch_yaw-Neutro_yaw) / 180.0;
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aux_float = (ch_yaw-yaw_mid) / 180.0;
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command_rx_yaw += aux_float;
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command_rx_yaw_diff = aux_float;
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@ -604,8 +661,9 @@ void loop(){
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// Quadcopter mix
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// Ask Jose if we still need this IF statement, and if we want to do an ESC calibration
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if (motorArmed == 1) {
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#ifdef IsAM
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digitalWrite(FR_LED, HIGH); // AM-Mode
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#endif
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#ifdef FLIGHT_MODE_+
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rightMotor = constrain(ch_throttle - control_roll - control_yaw, minThrottle, 2000);
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leftMotor = constrain(ch_throttle + control_roll - control_yaw, minThrottle, 2000);
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@ -620,7 +678,9 @@ void loop(){
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#endif
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}
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if (motorArmed == 0) {
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#ifdef IsAM
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digitalWrite(FR_LED, LOW); // AM-Mode
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#endif
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digitalWrite(LED_Green,HIGH); // Ready LED on
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rightMotor = MIN_THROTTLE;
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@ -674,7 +734,10 @@ void loop(){
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}
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}
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} // End of void loop()
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// END of Arducopter.pde
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}
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@ -135,8 +135,14 @@ void comma() {
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Serial.print(',');
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}
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||||
|
||||
#if BATTERY_EVENT == 1
|
||||
void low_battery_event(void)
|
||||
{
|
||||
// send_message(SEVERITY_HIGH,"Low Battery!");
|
||||
// set_mode(RTL);
|
||||
// throttle_cruise = THROTTLE_CRUISE;
|
||||
}
|
||||
#endif
|
||||
|
||||
|
||||
|
||||
|
|
|
|||
|
|
@ -33,27 +33,27 @@ void Position_control(long lat_dest, long lon_dest)
|
|||
// ROLL
|
||||
gps_err_roll_old = gps_err_roll;
|
||||
//Optimization : cos(yaw) = DCM_Matrix[0][0] ; sin(yaw) = DCM_Matrix[1][0]
|
||||
gps_err_roll = (float)Lon_diff*GEOG_CORRECTION_FACTOR*DCM_Matrix[0][0] - (float)Lat_diff*DCM_Matrix[1][0];
|
||||
gps_err_roll = (float)Lon_diff * GEOG_CORRECTION_FACTOR * DCM_Matrix[0][0] - (float)Lat_diff * DCM_Matrix[1][0];
|
||||
|
||||
gps_roll_D = (gps_err_roll-gps_err_roll_old)/GPS_Dt;
|
||||
gps_roll_D = (gps_err_roll-gps_err_roll_old) / GPS_Dt;
|
||||
|
||||
gps_roll_I += gps_err_roll*GPS_Dt;
|
||||
gps_roll_I = constrain(gps_roll_I,-800,800);
|
||||
gps_roll_I += gps_err_roll * GPS_Dt;
|
||||
gps_roll_I = constrain(gps_roll_I, -800, 800);
|
||||
|
||||
command_gps_roll = KP_GPS_ROLL*gps_err_roll + KD_GPS_ROLL*gps_roll_D + KI_GPS_ROLL*gps_roll_I;
|
||||
command_gps_roll = constrain(command_gps_roll,-GPS_MAX_ANGLE,GPS_MAX_ANGLE); // Limit max command
|
||||
command_gps_roll = KP_GPS_ROLL * gps_err_roll + KD_GPS_ROLL * gps_roll_D + KI_GPS_ROLL * gps_roll_I;
|
||||
command_gps_roll = constrain(command_gps_roll, -GPS_MAX_ANGLE, GPS_MAX_ANGLE); // Limit max command
|
||||
|
||||
// PITCH
|
||||
gps_err_pitch_old = gps_err_pitch;
|
||||
gps_err_pitch = -(float)Lat_diff*DCM_Matrix[0][0]- (float)Lon_diff*GEOG_CORRECTION_FACTOR*DCM_Matrix[1][0];
|
||||
gps_err_pitch = -(float)Lat_diff * DCM_Matrix[0][0] - (float)Lon_diff * GEOG_CORRECTION_FACTOR * DCM_Matrix[1][0];
|
||||
|
||||
gps_pitch_D = (gps_err_pitch-gps_err_pitch_old)/GPS_Dt;
|
||||
gps_pitch_D = (gps_err_pitch - gps_err_pitch_old) / GPS_Dt;
|
||||
|
||||
gps_pitch_I += gps_err_pitch*GPS_Dt;
|
||||
gps_pitch_I = constrain(gps_pitch_I,-800,800);
|
||||
gps_pitch_I += gps_err_pitch * GPS_Dt;
|
||||
gps_pitch_I = constrain(gps_pitch_I, -800, 800);
|
||||
|
||||
command_gps_pitch = KP_GPS_PITCH*gps_err_pitch + KD_GPS_PITCH*gps_pitch_D + KI_GPS_PITCH*gps_pitch_I;
|
||||
command_gps_pitch = constrain(command_gps_pitch,-GPS_MAX_ANGLE,GPS_MAX_ANGLE); // Limit max command
|
||||
command_gps_pitch = KP_GPS_PITCH * gps_err_pitch + KD_GPS_PITCH * gps_pitch_D + KI_GPS_PITCH * gps_pitch_I;
|
||||
command_gps_pitch = constrain(command_gps_pitch, -GPS_MAX_ANGLE, GPS_MAX_ANGLE); // Limit max command
|
||||
}
|
||||
|
||||
/* ************************************************************ */
|
||||
|
|
|
|||
|
|
@ -375,7 +375,7 @@ void sendSerialTelemetry() {
|
|||
case 'X': // Stop sending messages
|
||||
break;
|
||||
case '!': // Send flight software version
|
||||
Serial.println(SWVER);
|
||||
Serial.println(VER);
|
||||
queryType = 'X';
|
||||
break;
|
||||
case '.': // Modify GPS settings
|
||||
|
|
|
|||
|
|
@ -26,12 +26,13 @@ TODO:
|
|||
************************************************************* */
|
||||
|
||||
|
||||
|
||||
/*************************************************************/
|
||||
// Safety & Security
|
||||
|
||||
// Arm & Disarm delays
|
||||
#define ARM_DELAY 200
|
||||
#define DISARM_DELAY 100
|
||||
#define ARM_DELAY 200 // milliseconds of how long you need to keep rudder to max right for arming motors
|
||||
#define DISARM_DELAY 100 // milliseconds of how long you need to keep rudder to max left for disarming motors
|
||||
|
||||
|
||||
/*************************************************************/
|
||||
|
|
@ -57,10 +58,10 @@ TODO:
|
|||
|
||||
//#define RADIO_TEST_MODE
|
||||
|
||||
#define ROLL_MID 1478 // Radio Roll channel mid value
|
||||
#define PITCH_MID 1483 // Radio Pitch channel mid value
|
||||
#define ROLL_MID 1500 // Radio Roll channel mid value
|
||||
#define PITCH_MID 1500 // Radio Pitch channel mid value
|
||||
#define YAW_MID 1500 // Radio Yaw channel mid value
|
||||
#define THROTTLE_MID 1502 // Radio Throttle channel mid value
|
||||
#define THROTTLE_MID 1505 // Radio Throttle channel mid value
|
||||
#define AUX_MID 1500
|
||||
|
||||
#define CHANN_CENTER 1500 // Channel center, legacy
|
||||
|
|
@ -68,25 +69,25 @@ TODO:
|
|||
|
||||
// Following variables stored in EEPROM
|
||||
float KP_QUAD_ROLL;
|
||||
float KD_QUAD_ROLL;
|
||||
float KI_QUAD_ROLL;
|
||||
float KD_QUAD_ROLL;
|
||||
float KP_QUAD_PITCH;
|
||||
float KD_QUAD_PITCH;
|
||||
float KI_QUAD_PITCH;
|
||||
float KD_QUAD_PITCH;
|
||||
float KP_QUAD_YAW;
|
||||
float KD_QUAD_YAW;
|
||||
float KI_QUAD_YAW;
|
||||
float KD_QUAD_YAW;
|
||||
float STABLE_MODE_KP_RATE;
|
||||
float KP_GPS_ROLL;
|
||||
float KD_GPS_ROLL;
|
||||
float KI_GPS_ROLL;
|
||||
float KD_GPS_ROLL;
|
||||
float KP_GPS_PITCH;
|
||||
float KD_GPS_PITCH;
|
||||
float KI_GPS_PITCH;
|
||||
float KD_GPS_PITCH;
|
||||
float GPS_MAX_ANGLE;
|
||||
float KP_ALTITUDE;
|
||||
float KD_ALTITUDE;
|
||||
float KI_ALTITUDE;
|
||||
float KD_ALTITUDE;
|
||||
int acc_offset_x;
|
||||
int acc_offset_y;
|
||||
int acc_offset_z;
|
||||
|
|
@ -126,25 +127,25 @@ float ch_aux2_offset = 0;
|
|||
// when a "Default EEPROM Value" command is sent through serial interface
|
||||
void setUserConfig() {
|
||||
KP_QUAD_ROLL = 1.8;
|
||||
KD_QUAD_ROLL = 0.4; //0.48
|
||||
KI_QUAD_ROLL = 0.30; //0.4
|
||||
KD_QUAD_ROLL = 0.4; //0.48
|
||||
KP_QUAD_PITCH = 1.8;
|
||||
KD_QUAD_PITCH = 0.4; //0.48
|
||||
KI_QUAD_PITCH = 0.30; //0.4
|
||||
KD_QUAD_PITCH = 0.4; //0.48
|
||||
KP_QUAD_YAW = 3.6;
|
||||
KD_QUAD_YAW = 1.2;
|
||||
KI_QUAD_YAW = 0.15;
|
||||
KD_QUAD_YAW = 1.2;
|
||||
STABLE_MODE_KP_RATE = 0.2; // New param for stable mode
|
||||
KP_GPS_ROLL = 0.012;
|
||||
KD_GPS_ROLL = 0.005;
|
||||
KI_GPS_ROLL = 0.004;
|
||||
KP_GPS_PITCH = 0.012;
|
||||
KD_GPS_PITCH = 0.005;
|
||||
KI_GPS_PITCH = 0.004;
|
||||
GPS_MAX_ANGLE = 10;
|
||||
KP_GPS_ROLL = 0.02;
|
||||
KI_GPS_ROLL = 0.008;
|
||||
KD_GPS_ROLL = 0.006;
|
||||
KP_GPS_PITCH = 0.02;
|
||||
KI_GPS_PITCH = 0.008;
|
||||
KD_GPS_PITCH = 0.006;
|
||||
GPS_MAX_ANGLE = 18;
|
||||
KP_ALTITUDE = 0.8;
|
||||
KD_ALTITUDE = 0.2;
|
||||
KI_ALTITUDE = 0.2;
|
||||
KD_ALTITUDE = 0.2;
|
||||
acc_offset_x = 2073;
|
||||
acc_offset_y = 2056;
|
||||
acc_offset_z = 2010;
|
||||
|
|
@ -186,25 +187,25 @@ void setUserConfig() {
|
|||
|
||||
// EEPROM storage addresses
|
||||
#define KP_QUAD_ROLL_ADR 0
|
||||
#define KD_QUAD_ROLL_ADR 4
|
||||
#define KI_QUAD_ROLL_ADR 8
|
||||
#define KD_QUAD_ROLL_ADR 4
|
||||
#define KP_QUAD_PITCH_ADR 12
|
||||
#define KD_QUAD_PITCH_ADR 16
|
||||
#define KI_QUAD_PITCH_ADR 20
|
||||
#define KD_QUAD_PITCH_ADR 16
|
||||
#define KP_QUAD_YAW_ADR 24
|
||||
#define KD_QUAD_YAW_ADR 28
|
||||
#define KI_QUAD_YAW_ADR 32
|
||||
#define KD_QUAD_YAW_ADR 28
|
||||
#define STABLE_MODE_KP_RATE_ADR 36
|
||||
#define KP_GPS_ROLL_ADR 40
|
||||
#define KD_GPS_ROLL_ADR 44
|
||||
#define KI_GPS_ROLL_ADR 48
|
||||
#define KD_GPS_ROLL_ADR 44
|
||||
#define KP_GPS_PITCH_ADR 52
|
||||
#define KD_GPS_PITCH_ADR 56
|
||||
#define KI_GPS_PITCH_ADR 60
|
||||
#define KD_GPS_PITCH_ADR 56
|
||||
#define GPS_MAX_ANGLE_ADR 64
|
||||
#define KP_ALTITUDE_ADR 68
|
||||
#define KD_ALTITUDE_ADR 72
|
||||
#define KI_ALTITUDE_ADR 76
|
||||
#define KD_ALTITUDE_ADR 72
|
||||
#define acc_offset_x_ADR 80
|
||||
#define acc_offset_y_ADR 84
|
||||
#define acc_offset_z_ADR 88
|
||||
|
|
@ -268,25 +269,25 @@ void writeEEPROM(float value, int address) {
|
|||
|
||||
void readUserConfig() {
|
||||
KP_QUAD_ROLL = readEEPROM(KP_QUAD_ROLL_ADR);
|
||||
KD_QUAD_ROLL = readEEPROM(KD_QUAD_ROLL_ADR);
|
||||
KI_QUAD_ROLL = readEEPROM(KI_QUAD_ROLL_ADR);
|
||||
KD_QUAD_ROLL = readEEPROM(KD_QUAD_ROLL_ADR);
|
||||
KP_QUAD_PITCH = readEEPROM(KP_QUAD_PITCH_ADR);
|
||||
KD_QUAD_PITCH = readEEPROM(KD_QUAD_PITCH_ADR);
|
||||
KI_QUAD_PITCH = readEEPROM(KI_QUAD_PITCH_ADR);
|
||||
KD_QUAD_PITCH = readEEPROM(KD_QUAD_PITCH_ADR);
|
||||
KP_QUAD_YAW = readEEPROM(KP_QUAD_YAW_ADR);
|
||||
KD_QUAD_YAW = readEEPROM(KD_QUAD_YAW_ADR);
|
||||
KI_QUAD_YAW = readEEPROM(KI_QUAD_YAW_ADR);
|
||||
KD_QUAD_YAW = readEEPROM(KD_QUAD_YAW_ADR);
|
||||
STABLE_MODE_KP_RATE = readEEPROM(STABLE_MODE_KP_RATE_ADR);
|
||||
KP_GPS_ROLL = readEEPROM(KP_GPS_ROLL_ADR);
|
||||
KD_GPS_ROLL = readEEPROM(KD_GPS_ROLL_ADR);
|
||||
KI_GPS_ROLL = readEEPROM(KI_GPS_ROLL_ADR);
|
||||
KD_GPS_ROLL = readEEPROM(KD_GPS_ROLL_ADR);
|
||||
KP_GPS_PITCH = readEEPROM(KP_GPS_PITCH_ADR);
|
||||
KD_GPS_PITCH = readEEPROM(KD_GPS_PITCH_ADR);
|
||||
KI_GPS_PITCH = readEEPROM(KI_GPS_PITCH_ADR);
|
||||
KD_GPS_PITCH = readEEPROM(KD_GPS_PITCH_ADR);
|
||||
GPS_MAX_ANGLE = readEEPROM(GPS_MAX_ANGLE_ADR);
|
||||
KP_ALTITUDE = readEEPROM(KP_ALTITUDE_ADR);
|
||||
KD_ALTITUDE = readEEPROM(KD_ALTITUDE_ADR);
|
||||
KI_ALTITUDE = readEEPROM(KI_ALTITUDE_ADR);
|
||||
KD_ALTITUDE = readEEPROM(KD_ALTITUDE_ADR);
|
||||
acc_offset_x = readEEPROM(acc_offset_x_ADR);
|
||||
acc_offset_y = readEEPROM(acc_offset_y_ADR);
|
||||
acc_offset_z = readEEPROM(acc_offset_z_ADR);
|
||||
|
|
|
|||
Loading…
Reference in New Issue