// 2010 Jose Julio // 2011 Adapted 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 #if CH7_OPTION == CH7_FLIP void roll_flip() { #define AAP_THR_INC 180 #define AAP_THR_DEC 90 #define AAP_ROLL_OUT 200 #define AAP_ROLL_RATE 3000 // up to 1250 static int AAP_timer = 0; static byte AAP_state = 0; // Yaw g.rc_4.servo_out = get_stabilize_yaw(nav_yaw); // Pitch g.rc_2.servo_out = get_stabilize_pitch(0); // State machine switch (AAP_state){ case 0: // Step 1 : Initialize AAP_timer = 0; AAP_state++; break; case 1: // Step 2 : Increase throttle to start maneuver if (AAP_timer < 95){ // .5 seconds g.rc_1.servo_out = get_stabilize_roll(0); g.rc_3.servo_out = get_throttle(g.rc_3.control_in + AAP_THR_INC); //g.rc_4.servo_out = get_stabilize_yaw(nav_yaw); AAP_timer++; }else{ AAP_state++; AAP_timer = 0; } break; case 2: // Step 3 : ROLL (until we reach a certain angle [45º]) if (dcm.roll_sensor < 4500){ // Roll control g.rc_1.servo_out = AAP_ROLL_OUT; //get_rate_roll(AAP_ROLL_RATE); g.rc_3.servo_out = get_throttle(g.rc_3.control_in - AAP_THR_DEC); }else{ AAP_state++; } break; case 3: // Step 4 : CONTINUE ROLL (until we reach a certain angle [-45º]) if ((dcm.roll_sensor >= 4500) || (dcm.roll_sensor < -4500)){ g.rc_1.servo_out = 150; //get_rate_roll(AAP_ROLL_RATE); g.rc_3.servo_out = get_throttle(g.rc_3.control_in - AAP_THR_DEC); }else{ AAP_state++; } break; case 4: // Step 5 : Increase throttle to stop the descend if (AAP_timer < 90){ // .5 seconds g.rc_1.servo_out = get_stabilize_roll(0); g.rc_3.servo_out = get_throttle(g.rc_3.control_in + AAP_THR_INC); AAP_timer++; }else{ AAP_state++; AAP_timer = 0; } break; case 5: // exit mode //control_mode = do_flip = false; break; } } #endif