//////////////////////////////////////////////////////////////////////////////// // Toy Mode - THOR //////////////////////////////////////////////////////////////////////////////// static boolean CH7_toy_flag; static boolean CH6_toy_flag; static int16_t saved_toy_throttle; #if TOY_MIXER == TOY_LOOKUP_TABLE static const int16_t toy_lookup[] = { 186, 373, 558, 745, 372, 745, 1117, 1490, 558, 1118, 1675, 2235, 743, 1490, 2233, 2980, 929, 1863, 2792, 3725, 1115, 2235, 3350, 4470, 1301, 2608, 3908, 4500, 1487, 2980, 4467, 4500, 1673, 3353, 4500, 4500}; #endif //called at 10hz void update_toy_throttle() { if (false == CH6_toy_flag && g.rc_6.radio_in >= CH_6_PWM_TRIGGER){ CH6_toy_flag = true; throttle_mode = THROTTLE_MANUAL; }else if (CH6_toy_flag && g.rc_6.radio_in < CH_6_PWM_TRIGGER){ CH6_toy_flag = false; throttle_mode = THROTTLE_AUTO; set_new_altitude(current_loc.alt); saved_toy_throttle = g.rc_3.control_in; } // look for a change in throttle position to exit throttle hold if(abs(g.rc_3.control_in - saved_toy_throttle) > 40){ throttle_mode = THROTTLE_MANUAL; } } #define TOY_ALT_SMALL 25 #define TOY_ALT_LARGE 100 //called at 10hz void update_toy_altitude() { int16_t input = g.rc_3.radio_in; // throttle //int16_t input = g.rc_7.radio_in; // Trigger upward alt change if(false == CH7_toy_flag && input > 1666){ CH7_toy_flag = true; // go up if(next_WP.alt >= 400){ force_new_altitude(next_WP.alt + TOY_ALT_LARGE); }else{ force_new_altitude(next_WP.alt + TOY_ALT_SMALL); } // Trigger downward alt change }else if(false == CH7_toy_flag && input < 1333){ CH7_toy_flag = true; // go down if(next_WP.alt >= (400 + TOY_ALT_LARGE)){ force_new_altitude(next_WP.alt - TOY_ALT_LARGE); }else if(next_WP.alt >= TOY_ALT_SMALL){ force_new_altitude(next_WP.alt - TOY_ALT_SMALL); }else if(next_WP.alt < TOY_ALT_SMALL){ force_new_altitude(0); } // clear flag }else if (CH7_toy_flag && ((input < 1666) && (input > 1333))){ CH7_toy_flag = false; } } // called at 50 hz from all flight modes #if TOY_EDF == ENABLED void edf_toy() { // EDF control: g.rc_8.radio_out = 1000 + ((abs(g.rc_2.control_in) << 1) / 9); if(g.rc_8.radio_out < 1050) g.rc_8.radio_out = 1000; // output throttle to EDF if(motors.armed()){ APM_RC.OutputCh(CH_8, g.rc_8.radio_out); }else{ APM_RC.OutputCh(CH_8, 1000); } // output Servo direction if(g.rc_2.control_in > 0){ APM_RC.OutputCh(CH_6, 1000); // 1000 : 2000 }else{ APM_RC.OutputCh(CH_6, 2000); // less than 1450 } } #endif // The function call for managing the flight mode Toy void roll_pitch_toy() { #if TOY_MIXER == TOY_LOOKUP_TABLE || TOY_MIXER == TOY_LINEAR_MIXER int16_t yaw_rate = g.rc_1.control_in / g.toy_yaw_rate; if(g.rc_1.control_in != 0){ // roll g.rc_4.servo_out = get_acro_yaw(yaw_rate/2); yaw_stopped = false; yaw_timer = 150; }else if (!yaw_stopped){ g.rc_4.servo_out = get_acro_yaw(0); yaw_timer--; if((yaw_timer == 0) || (fabs(omega.z) < .17)){ yaw_stopped = true; nav_yaw = ahrs.yaw_sensor; } }else{ if(motors.armed() == false || g.rc_3.control_in == 0) nav_yaw = ahrs.yaw_sensor; g.rc_4.servo_out = get_stabilize_yaw(nav_yaw); } #endif // roll_rate is the outcome of the linear equation or lookup table // based on speed and Yaw rate int16_t roll_rate = 0; #if TOY_MIXER == TOY_LOOKUP_TABLE uint8_t xx, yy; // Lookup value //xx = g_gps->ground_speed / 200; xx = abs(g.rc_2.control_in / 1000); yy = abs(yaw_rate / 500); // constrain to lookup Array range xx = constrain(xx, 0, 3); yy = constrain(yy, 0, 8); roll_rate = toy_lookup[yy * 4 + xx]; if(yaw_rate == 0){ roll_rate = 0; }else if(yaw_rate < 0){ roll_rate = -roll_rate; } int16_t roll_limit = 4500 / g.toy_yaw_rate; roll_rate = constrain(roll_rate, -roll_limit, roll_limit); #elif TOY_MIXER == TOY_LINEAR_MIXER roll_rate = -((int32_t)g.rc_2.control_in * (yaw_rate/100)) /30; //Serial.printf("roll_rate: %d\n",roll_rate); roll_rate = constrain(roll_rate, -2000, 2000); #elif TOY_MIXER == TOY_EXTERNAL_MIXER // JKR update to allow external roll/yaw mixing roll_rate = g.rc_1.control_in; #endif #if TOY_EDF == ENABLED // Output the attitude g.rc_1.servo_out = get_stabilize_roll(roll_rate); g.rc_2.servo_out = get_stabilize_pitch(0); #else // Output the attitude g.rc_1.servo_out = get_stabilize_roll(roll_rate); g.rc_2.servo_out = get_stabilize_pitch(g.rc_2.control_in); #endif }