// 2010 Jose Julio // 2011 Adapted and updated for AC2 by Jason Short // // Automatic Acrobatic Procedure (AAP) v1 : Roll flip // State machine aproach: // Some states are fixed commands (for a fixed time) // Some states are fixed commands (until some IMU condition) // Some states include controls inside uint8_t flip_timer; uint8_t flip_state; #define AAP_THR_INC 170 #define AAP_THR_DEC 90 #define AAP_ROLL_OUT 2000 void init_flip() { if(do_flip == false){ do_flip = true; flip_timer = 0; flip_state = 0; } } void roll_flip() { // Yaw g.rc_4.servo_out = get_stabilize_yaw(nav_yaw); // Pitch g.rc_2.servo_out = get_stabilize_pitch(0); // Roll State machine switch (flip_state){ case 0: // Step 1 : Initialize flip_timer = 0; flip_state++; break; case 1: // Step 2 : Increase throttle to start maneuver if (flip_timer < 90){ // .5 seconds g.rc_1.servo_out = get_stabilize_roll(0); g.rc_3.servo_out = g.throttle_cruise + AAP_THR_INC; flip_timer++; }else{ flip_state++; flip_timer = 0; } break; case 2: // Step 3 : ROLL (until we reach a certain angle [45deg]) if (ahrs.roll_sensor < 4500){ // Roll control g.rc_1.servo_out = AAP_ROLL_OUT; g.rc_3.servo_out = g.throttle_cruise; }else{ flip_state++; } break; case 3: // Step 4 : CONTINUE ROLL (until we reach a certain angle [-45deg]) if((ahrs.roll_sensor >= 4500) || (ahrs.roll_sensor < -9000)){// we are in second half of roll //g.rc_1.servo_out = 0; g.rc_1.servo_out = get_rate_roll(40000); g.rc_3.servo_out = g.throttle_cruise - AAP_THR_DEC; }else{ flip_state++; } break; case 4: // Step 5 : Increase throttle to stop the descend if (flip_timer < 120){ // .5 seconds g.rc_1.servo_out = get_stabilize_roll(0); g.rc_3.servo_out = g.throttle_cruise + g.throttle_cruise / 2; flip_timer++; }else{ flip_state++; flip_timer = 0; } break; case 5: // exit mode flip_timer = 0; flip_state = 0; do_flip = false; break; } }