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ardupilot/ArducopterNG/GCS.pde

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/*
www.ArduCopter.com - www.DIYDrones.com
Copyright (c) 2010. All rights reserved.
An Open Source Arduino based multicopter.
File : GCS.pde
Version : v1.0, Aug 27, 2010
Author(s): ArduCopter Team
Ted Carancho (aeroquad), Jose Julio, Jordi Muñoz,
Jani Hirvinen, Ken McEwans, Roberto Navoni,
Sandro Benigno, Chris Anderson
This program is free software: you can redistribute it and/or modify
it 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.
This program is distributed in the hope that it 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 program. If not, see <http://www.gnu.org/licenses/>.
* ************************************************************** *
ChangeLog:
* ************************************************************** *
TODO:
* ************************************************************** */
//
// Function : send_message()
//
// Parameters:
// byte severity - Debug level
// char str - Text to write
//
// Returns : - none
void send_message(byte severity, const char *str) // This is the instance of send_message for message 0x05
{
if(severity >= DEBUG_LEVEL){
SerPr("MSG: ");
SerPrln(str);
}
}
//////////////////////////////////////////////////
// Function : readSerialCommand()
//
// Parameters:
// - none
//
// Returns : - none
//
void readSerialCommand() {
// Check for serial message
if (SerAv()) {
queryType = SerRe();
switch (queryType) {
case 'A': // Stable PID
KP_QUAD_ROLL = readFloatSerial();
KI_QUAD_ROLL = readFloatSerial();
STABLE_MODE_KP_RATE_ROLL = readFloatSerial();
KP_QUAD_PITCH = readFloatSerial();
KI_QUAD_PITCH = readFloatSerial();
STABLE_MODE_KP_RATE_PITCH = readFloatSerial();
KP_QUAD_YAW = readFloatSerial();
KI_QUAD_YAW = readFloatSerial();
STABLE_MODE_KP_RATE_YAW = readFloatSerial();
STABLE_MODE_KP_RATE = readFloatSerial(); // NOT USED NOW
MAGNETOMETER = readFloatSerial();
break;
case 'C': // Receive GPS PID
KP_GPS_ROLL = readFloatSerial();
KI_GPS_ROLL = readFloatSerial();
KD_GPS_ROLL = readFloatSerial();
KP_GPS_PITCH = readFloatSerial();
KI_GPS_PITCH = readFloatSerial();
KD_GPS_PITCH = readFloatSerial();
GPS_MAX_ANGLE = readFloatSerial();
GEOG_CORRECTION_FACTOR = readFloatSerial();
break;
case 'E': // Receive altitude PID
KP_ALTITUDE = readFloatSerial();
KD_ALTITUDE = readFloatSerial();
KI_ALTITUDE = readFloatSerial();
break;
case 'G': // Receive drift correction PID
Kp_ROLLPITCH = readFloatSerial();
Ki_ROLLPITCH = readFloatSerial();
Kp_YAW = readFloatSerial();
Ki_YAW = readFloatSerial();
break;
case 'I': // Receive sensor offset
gyro_offset_roll = readFloatSerial();
gyro_offset_pitch = readFloatSerial();
gyro_offset_yaw = readFloatSerial();
acc_offset_x = readFloatSerial();
acc_offset_y = readFloatSerial();
acc_offset_z = readFloatSerial();
break;
case 'K': // Spare
break;
case 'M': // Receive debug motor commands
frontMotor = readFloatSerial();
backMotor = readFloatSerial();
rightMotor = readFloatSerial();
leftMotor = readFloatSerial();
motorArmed = readFloatSerial();
break;
case 'O': // Rate Control PID
Kp_RateRoll = readFloatSerial();
Ki_RateRoll = readFloatSerial();
Kd_RateRoll = readFloatSerial();
Kp_RatePitch = readFloatSerial();
Ki_RatePitch = readFloatSerial();
Kd_RatePitch = readFloatSerial();
Kp_RateYaw = readFloatSerial();
Ki_RateYaw = readFloatSerial();
Kd_RateYaw = readFloatSerial();
xmitFactor = readFloatSerial();
break;
case 'W': // Write all user configurable values to EEPROM
writeUserConfig();
break;
case 'Y': // Initialize EEPROM with default values
defaultUserConfig();
break;
case '1': // Receive transmitter calibration values
ch_roll_slope = readFloatSerial();
ch_roll_offset = readFloatSerial();
ch_pitch_slope = readFloatSerial();
ch_pitch_offset = readFloatSerial();
ch_yaw_slope = readFloatSerial();
ch_yaw_offset = readFloatSerial();
ch_throttle_slope = readFloatSerial();
ch_throttle_offset = readFloatSerial();
ch_aux_slope = readFloatSerial();
ch_aux_offset = readFloatSerial();
ch_aux2_slope = readFloatSerial();
ch_aux2_offset = readFloatSerial();
break;
}
}
}
void sendSerialTelemetry() {
float aux_float[3]; // used for sensor calibration
switch (queryType) {
case '=': // Reserved debug command to view any variable from Serial Monitor
/* SerPr("throttle =");
SerPrln(ch_throttle);
SerPr("control roll =");
SerPrln(control_roll-CHANN_CENTER);
SerPr("control pitch =");
SerPrln(control_pitch-CHANN_CENTER);
SerPr("control yaw =");
SerPrln(control_yaw-CHANN_CENTER);
SerPr("front left yaw =");
SerPrln(frontMotor);
SerPr("front right yaw =");
SerPrln(rightMotor);
SerPr("rear left yaw =");
SerPrln(leftMotor);
SerPr("rear right motor =");
SerPrln(backMotor);
SerPrln();
SerPr("current roll rate =");
SerPrln(read_adc(0));
SerPr("current pitch rate =");
SerPrln(read_adc(1));
SerPr("current yaw rate =");
SerPrln(read_adc(2));
SerPr("command rx yaw =");
SerPrln(command_rx_yaw);
SerPrln();
queryType = 'X';*/
SerPr(APM_RC.InputCh(0));
comma();
SerPr(ch_roll_slope);
comma();
SerPr(ch_roll_offset);
comma();
SerPrln(ch_roll);
break;
case 'B': // Send roll, pitch and yaw PID values
SerPr(KP_QUAD_ROLL, 3);
comma();
SerPr(KI_QUAD_ROLL, 3);
comma();
SerPr(STABLE_MODE_KP_RATE_ROLL, 3);
comma();
SerPr(KP_QUAD_PITCH, 3);
comma();
SerPr(KI_QUAD_PITCH, 3);
comma();
SerPr(STABLE_MODE_KP_RATE_PITCH, 3);
comma();
SerPr(KP_QUAD_YAW, 3);
comma();
SerPr(KI_QUAD_YAW, 3);
comma();
SerPr(STABLE_MODE_KP_RATE_YAW, 3);
comma();
SerPr(STABLE_MODE_KP_RATE, 3); // NOT USED NOW
comma();
SerPrln(MAGNETOMETER, 3);
queryType = 'X';
break;
case 'D': // Send GPS PID
SerPr(KP_GPS_ROLL, 3);
comma();
SerPr(KI_GPS_ROLL, 3);
comma();
SerPr(KD_GPS_ROLL, 3);
comma();
SerPr(KP_GPS_PITCH, 3);
comma();
SerPr(KI_GPS_PITCH, 3);
comma();
SerPr(KD_GPS_PITCH, 3);
comma();
SerPr(GPS_MAX_ANGLE, 3);
comma();
SerPrln(GEOG_CORRECTION_FACTOR, 3);
queryType = 'X';
break;
case 'F': // Send altitude PID
SerPr(KP_ALTITUDE, 3);
comma();
SerPr(KI_ALTITUDE, 3);
comma();
SerPrln(KD_ALTITUDE, 3);
queryType = 'X';
break;
case 'H': // Send drift correction PID
SerPr(Kp_ROLLPITCH, 4);
comma();
SerPr(Ki_ROLLPITCH, 7);
comma();
SerPr(Kp_YAW, 4);
comma();
SerPrln(Ki_YAW, 6);
queryType = 'X';
break;
case 'J': // Send sensor offset
SerPr(gyro_offset_roll);
comma();
SerPr(gyro_offset_pitch);
comma();
SerPr(gyro_offset_yaw);
comma();
SerPr(acc_offset_x);
comma();
SerPr(acc_offset_y);
comma();
SerPrln(acc_offset_z);
AN_OFFSET[3] = acc_offset_x;
AN_OFFSET[4] = acc_offset_y;
AN_OFFSET[5] = acc_offset_z;
queryType = 'X';
break;
case 'L': // Spare
// RadioCalibration();
queryType = 'X';
break;
case 'N': // Send magnetometer config
queryType = 'X';
break;
case 'P': // Send rate control PID
SerPr(Kp_RateRoll, 3);
comma();
SerPr(Ki_RateRoll, 3);
comma();
SerPr(Kd_RateRoll, 3);
comma();
SerPr(Kp_RatePitch, 3);
comma();
SerPr(Ki_RatePitch, 3);
comma();
SerPr(Kd_RatePitch, 3);
comma();
SerPr(Kp_RateYaw, 3);
comma();
SerPr(Ki_RateYaw, 3);
comma();
SerPr(Kd_RateYaw, 3);
comma();
SerPrln(xmitFactor, 3);
queryType = 'X';
break;
case 'Q': // Send sensor data
SerPr(read_adc(0));
comma();
SerPr(read_adc(1));
comma();
SerPr(read_adc(2));
comma();
SerPr(read_adc(4));
comma();
SerPr(read_adc(3));
comma();
SerPr(read_adc(5));
comma();
SerPr(err_roll);
comma();
SerPr(err_pitch);
comma();
SerPr(degrees(roll));
comma();
SerPr(degrees(pitch));
comma();
SerPrln(degrees(yaw));
break;
case 'R': // Send raw sensor data
break;
case 'S': // Send all flight data
SerPr(timer-timer_old);
comma();
SerPr(read_adc(0));
comma();
SerPr(read_adc(1));
comma();
SerPr(read_adc(2));
comma();
SerPr(ch_throttle);
comma();
SerPr(control_roll);
comma();
SerPr(control_pitch);
comma();
SerPr(control_yaw);
comma();
SerPr(frontMotor); // Front Motor
comma();
SerPr(backMotor); // Back Motor
comma();
SerPr(rightMotor); // Right Motor
comma();
SerPr(leftMotor); // Left Motor
comma();
SerPr(read_adc(4));
comma();
SerPr(read_adc(3));
comma();
SerPrln(read_adc(5));
break;
case 'T': // Spare
break;
case 'U': // Send receiver values
SerPr(ch_roll); // Aileron
comma();
SerPr(ch_pitch); // Elevator
comma();
SerPr(ch_yaw); // Yaw
comma();
SerPr(ch_throttle); // Throttle
comma();
SerPr(ch_aux); // AUX1 (Mode)
comma();
SerPr(ch_aux2); // AUX2
comma();
SerPr(roll_mid); // Roll MID value
comma();
SerPr(pitch_mid); // Pitch MID value
comma();
SerPrln(yaw_mid); // Yaw MID Value
break;
case 'V': // Spare
break;
case 'X': // Stop sending messages
break;
case '!': // Send flight software version
SerPrln(VER);
queryType = 'X';
break;
case '2': // Send transmitter calibration values
SerPr(ch_roll_slope);
comma();
SerPr(ch_roll_offset);
comma();
SerPr(ch_pitch_slope);
comma();
SerPr(ch_pitch_offset);
comma();
SerPr(ch_yaw_slope);
comma();
SerPr(ch_yaw_offset);
comma();
SerPr(ch_throttle_slope);
comma();
SerPr(ch_throttle_offset);
comma();
SerPr(ch_aux_slope);
comma();
SerPr(ch_aux_offset);
comma();
SerPr(ch_aux2_slope);
comma();
SerPrln(ch_aux2_offset);
queryType = 'X';
break;
case '.': // Modify GPS settings, print directly to GPS Port
Serial1.print("$PGCMD,16,0,0,0,0,0*6A\r\n");
break;
}
}
void comma() {
SerPr(',');
}
// Used to read floating point values from the serial port
float readFloatSerial() {
byte index = 0;
byte timeout = 0;
char data[128] = "";
do {
if (SerAv() == 0) {
delay(10);
timeout++;
}
else {
data[index] = SerRe();
timeout = 0;
index++;
}
}
while ((data[constrain(index-1, 0, 128)] != ';') && (timeout < 5) && (index < 128));
return atof(data);
}
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