#include "board.h" #include "mw.h" static uint8_t numberMotor = 4; int16_t motor[8]; int16_t servo[8] = { 1500, 1500, 1500, 1500, 1500, 1500, 1500, 1500 }; uint8_t mixerConfiguration = MULTITYPE_TRI; uint16_t wing_left_mid = WING_LEFT_MID; uint16_t wing_right_mid = WING_RIGHT_MID; uint16_t tri_yaw_middle = TRI_YAW_MIDDLE; void mixerInit(void) { if (mixerConfiguration == MULTITYPE_BI || mixerConfiguration == MULTITYPE_TRI || mixerConfiguration == MULTITYPE_GIMBAL || mixerConfiguration == MULTITYPE_FLYING_WING) featureSet(FEATURE_SERVO); switch (mixerConfiguration) { case MULTITYPE_GIMBAL: numberMotor = 0; break; case MULTITYPE_FLYING_WING: numberMotor = 1; break; case MULTITYPE_BI: numberMotor = 2; break; case MULTITYPE_TRI: numberMotor = 3; break; case MULTITYPE_QUADP: case MULTITYPE_QUADX: case MULTITYPE_Y4: case MULTITYPE_VTAIL4: numberMotor = 4; break; case MULTITYPE_Y6: case MULTITYPE_HEX6: case MULTITYPE_HEX6X: numberMotor = 6; break; case MULTITYPE_OCTOX8: case MULTITYPE_OCTOFLATP: case MULTITYPE_OCTOFLATX: numberMotor = 8; break; } } void writeServos(void) { if (!feature(FEATURE_SERVO)) return; if (mixerConfiguration == MULTITYPE_TRI || mixerConfiguration == MULTITYPE_BI) { /* One servo on Motor #4 */ pwmWrite(0, servo[4]); if (mixerConfiguration == MULTITYPE_BI) pwmWrite(1, servo[5]); } else { /* Two servos for camstab or FLYING_WING */ pwmWrite(0, servo[0]); pwmWrite(1, servo[1]); } } void writeMotors(void) { uint8_t i; uint8_t offset = 0; // when servos are enabled, motor outputs 1..2 are for servos only if (feature(FEATURE_SERVO)) offset = 2; for (i = 0; i < numberMotor; i++) pwmWrite(i + offset, motor[i]); } void writeAllMotors(int16_t mc) { uint8_t i; // Sends commands to all motors for (i = 0; i < numberMotor; i++) motor[i] = mc; writeMotors(); } #define PIDMIX(X,Y,Z) rcCommand[THROTTLE] + axisPID[ROLL] * X + axisPID[PITCH] * Y + YAW_DIRECTION * axisPID[YAW] * Z void mixTable(void) { int16_t maxMotor; uint8_t i, axis; static uint8_t camCycle = 0; static uint8_t camState = 0; static uint32_t camTime = 0; if (numberMotor > 3) { //prevent "yaw jump" during yaw correction axisPID[YAW] = constrain(axisPID[YAW], -100 - abs(rcCommand[YAW]), +100 + abs(rcCommand[YAW])); } switch (mixerConfiguration) { case MULTITYPE_BI: motor[0] = PIDMIX(+1, 0, 0); //LEFT motor[1] = PIDMIX(-1, 0, 0); //RIGHT servo[4] = constrain(1500 + YAW_DIRECTION * (axisPID[YAW] + axisPID[PITCH]), 1020, 2000); //LEFT servo[5] = constrain(1500 + YAW_DIRECTION * (axisPID[YAW] - axisPID[PITCH]), 1020, 2000); //RIGHT break; case MULTITYPE_TRI: motor[0] = PIDMIX(0, +4 / 3, 0); //REAR motor[1] = PIDMIX(-1, -2 / 3, 0); //RIGHT motor[2] = PIDMIX(+1, -2 / 3, 0); //LEFT servo[4] = constrain(tri_yaw_middle + YAW_DIRECTION * axisPID[YAW], TRI_YAW_CONSTRAINT_MIN, TRI_YAW_CONSTRAINT_MAX); //REAR break; case MULTITYPE_QUADP: motor[0] = PIDMIX(0, +1, -1); //REAR motor[1] = PIDMIX(-1, 0, +1); //RIGHT motor[2] = PIDMIX(+1, 0, +1); //LEFT motor[3] = PIDMIX(0, -1, -1); //FRONT break; case MULTITYPE_QUADX: motor[0] = PIDMIX(-1, +1, -1); //REAR_R motor[1] = PIDMIX(-1, -1, +1); //FRONT_R motor[2] = PIDMIX(+1, +1, +1); //REAR_L motor[3] = PIDMIX(+1, -1, -1); //FRONT_L break; case MULTITYPE_Y4: motor[0] = PIDMIX(+0, +1, -1); //REAR_1 CW motor[1] = PIDMIX(-1, -1, 0); //FRONT_R CCW motor[2] = PIDMIX(+0, +1, +1); //REAR_2 CCW motor[3] = PIDMIX(+1, -1, 0); //FRONT_L CW break; case MULTITYPE_Y6: motor[0] = PIDMIX(+0, +4 / 3, +1); //REAR motor[1] = PIDMIX(-1, -2 / 3, -1); //RIGHT motor[2] = PIDMIX(+1, -2 / 3, -1); //LEFT motor[3] = PIDMIX(+0, +4 / 3, -1); //UNDER_REAR motor[4] = PIDMIX(-1, -2 / 3, +1); //UNDER_RIGHT motor[5] = PIDMIX(+1, -2 / 3, +1); //UNDER_LEFT break; case MULTITYPE_HEX6: motor[0] = PIDMIX(-1 / 2, +1 / 2, +1); //REAR_R motor[1] = PIDMIX(-1 / 2, -1 / 2, -1); //FRONT_R motor[2] = PIDMIX(+1 / 2, +1 / 2, +1); //REAR_L motor[3] = PIDMIX(+1 / 2, -1 / 2, -1); //FRONT_L motor[4] = PIDMIX(+0, -1, +1); //FRONT motor[5] = PIDMIX(+0, +1, -1); //REAR break; case MULTITYPE_HEX6X: motor[0] = PIDMIX(-1 / 2, +1 / 2, +1); //REAR_R motor[1] = PIDMIX(-1 / 2, -1 / 2, +1); //FRONT_R motor[2] = PIDMIX(+1 / 2, +1 / 2, -1); //REAR_L motor[3] = PIDMIX(+1 / 2, -1 / 2, -1); //FRONT_L motor[4] = PIDMIX(-1, +0, -1); //RIGHT motor[5] = PIDMIX(+1, +0, +1); //LEFT break; case MULTITYPE_OCTOX8: motor[0] = PIDMIX(-1, +1, -1); //REAR_R motor[1] = PIDMIX(-1, -1, +1); //FRONT_R motor[2] = PIDMIX(+1, +1, +1); //REAR_L motor[3] = PIDMIX(+1, -1, -1); //FRONT_L motor[4] = PIDMIX(-1, +1, +1); //UNDER_REAR_R motor[5] = PIDMIX(-1, -1, -1); //UNDER_FRONT_R motor[6] = PIDMIX(+1, +1, -1); //UNDER_REAR_L motor[7] = PIDMIX(+1, -1, +1); //UNDER_FRONT_L break; case MULTITYPE_OCTOFLATP: motor[0] = PIDMIX(+7 / 10, -7 / 10, +1); //FRONT_L motor[1] = PIDMIX(-7 / 10, -7 / 10, +1); //FRONT_R motor[2] = PIDMIX(-7 / 10, +7 / 10, +1); //REAR_R motor[3] = PIDMIX(+7 / 10, +7 / 10, +1); //REAR_L motor[4] = PIDMIX(+0, -1, -1); //FRONT motor[5] = PIDMIX(-1, +0, -1); //RIGHT motor[6] = PIDMIX(+0, +1, -1); //REAR motor[7] = PIDMIX(+1, +0, -1); //LEFT break; case MULTITYPE_OCTOFLATX: motor[0] = PIDMIX(+1, -1 / 2, +1); //MIDFRONT_L motor[1] = PIDMIX(-1 / 2, -1, +1); //FRONT_R motor[2] = PIDMIX(-1, +1 / 2, +1); //MIDREAR_R motor[3] = PIDMIX(+1 / 2, +1, +1); //REAR_L motor[4] = PIDMIX(+1 / 2, -1, -1); //FRONT_L motor[5] = PIDMIX(-1, -1 / 2, -1); //MIDFRONT_R motor[6] = PIDMIX(-1 / 2, +1, -1); //REAR_R motor[7] = PIDMIX(+1, +1 / 2, -1); //MIDREAR_L break; case MULTITYPE_VTAIL4: motor[0] = PIDMIX(+0, +1, -1 / 2); //REAR_R motor[1] = PIDMIX(-1, -1, +2 / 10); //FRONT_R motor[2] = PIDMIX(+0, +1, +1 / 2); //REAR_L motor[3] = PIDMIX(+1, -1, -2 / 10); //FRONT_L break; case MULTITYPE_GIMBAL: servo[0] = constrain(TILT_PITCH_MIDDLE + TILT_PITCH_PROP * angle[PITCH] / 16 + rcCommand[PITCH], TILT_PITCH_MIN, TILT_PITCH_MAX); servo[1] = constrain(TILT_ROLL_MIDDLE + TILT_ROLL_PROP * angle[ROLL] / 16 + rcCommand[ROLL], TILT_ROLL_MIN, TILT_ROLL_MAX); break; case MULTITYPE_FLYING_WING: motor[0] = rcCommand[THROTTLE]; if (passThruMode) { // do not use sensors for correction, simple 2 channel mixing servo[0] = PITCH_DIRECTION_L * (rcData[PITCH] - MIDRC) + ROLL_DIRECTION_L * (rcData[ROLL] - MIDRC); servo[1] = PITCH_DIRECTION_R * (rcData[PITCH] - MIDRC) + ROLL_DIRECTION_R * (rcData[ROLL] - MIDRC); } else { // use sensors to correct (gyro only or gyro+acc according to aux1/aux2 configuration servo[0] = PITCH_DIRECTION_L * axisPID[PITCH] + ROLL_DIRECTION_L * axisPID[ROLL]; servo[1] = PITCH_DIRECTION_R * axisPID[PITCH] + ROLL_DIRECTION_R * axisPID[ROLL]; } servo[0] = constrain(servo[0] + wing_left_mid , WING_LEFT_MIN, WING_LEFT_MAX); servo[1] = constrain(servo[1] + wing_right_mid, WING_RIGHT_MIN, WING_RIGHT_MAX); break; } #ifdef SERVO_TILT servo[0] = TILT_PITCH_MIDDLE + rcData[AUX3] - 1500; servo[1] = TILT_ROLL_MIDDLE + rcData[AUX4] - 1500; if (rcOptions[BOXCAMSTAB]) { servo[0] += TILT_PITCH_PROP * angle[PITCH] / 16; servo[1] += TILT_ROLL_PROP * angle[ROLL] / 16; } servo[0] = constrain(servo[0], TILT_PITCH_MIN, TILT_PITCH_MAX); servo[1] = constrain(servo[1], TILT_ROLL_MIN, TILT_ROLL_MAX); #endif #if defined(CAMTRIG) if (camCycle == 1) { if (camState == 0) { servo[2] = CAM_SERVO_HIGH; camState = 1; camTime = millis(); } else if (camState == 1) { if ((millis() - camTime) > CAM_TIME_HIGH) { servo[2] = CAM_SERVO_LOW; camState = 2; camTime = millis(); } } else { //camState ==2 if ((millis() - camTime) > CAM_TIME_LOW) { camState = 0; camCycle = 0; } } } if (rcOptions[BOXCAMTRIG]) camCycle = 1; #endif maxMotor = motor[0]; for (i = 1; i < numberMotor; i++) if (motor[i] > maxMotor) maxMotor = motor[i]; for (i = 0; i < numberMotor; i++) { if (maxMotor > MAXTHROTTLE) // this is a way to still have good gyro corrections if at least one motor reaches its max. motor[i] -= maxMotor - MAXTHROTTLE; motor[i] = constrain(motor[i], MINTHROTTLE, MAXTHROTTLE); if ((rcData[THROTTLE]) < MINCHECK) #ifndef MOTOR_STOP motor[i] = MINTHROTTLE; #else motor[i] = MINCOMMAND; #endif if (armed == 0) motor[i] = MINCOMMAND; } #if (LOG_VALUES == 2) || defined(POWERMETER_SOFT) uint32_t amp; /* true cubic function; when divided by vbat_max=126 (12.6V) for 3 cell battery this gives maximum value of ~ 500 */ /* Lookup table moved to PROGMEM 11/21/2001 by Danal */ static uint16_t amperes[64] = { 0, 2, 6, 15, 30, 52, 82, 123, 175, 240, 320, 415, 528, 659, 811, 984, 1181, 1402, 1648, 1923, 2226, 2559, 2924, 3322, 3755, 4224, 4730, 5276, 5861, 6489, 7160, 7875, 8637, 9446, 10304, 11213, 12173, 13187, 14256, 15381, 16564, 17805, 19108, 20472, 21900, 23392, 24951, 26578, 28274, 30041, 31879, 33792, 35779, 37843, 39984, 42205, 44507, 46890, 49358, 51910, 54549, 57276, 60093, 63000}; if (vbat) { // by all means - must avoid division by zero for (i = 0; i < NUMBER_MOTOR; i++) { amp = amperes[((motor[i] - 1000) >> 4)] / vbat; // range mapped from [1000:2000] => [0:1000]; then break that up into 64 ranges; lookup amp #if (LOG_VALUES == 2) pMeter[i] += amp; // sum up over time the mapped ESC input #endif #if defined(POWERMETER_SOFT) pMeter[PMOTOR_SUM] += amp; // total sum over all motors #endif } } #endif }