Subversion Repositories FlightCtrl

Rev

Rev 2135 | Rev 2142 | Go to most recent revision | Show entire file | Ignore whitespace | Details | Blame | Last modification | View Log | RSS feed

Rev 2135 Rev 2138
Line 262... Line 262...
262 
                debugOut.analog[8] = target[YAW] / (GYRO_DEG_FACTOR / 10);
 262 
                debugOut.analog[8] = target[YAW] / (GYRO_DEG_FACTOR / 10);
Line 263... Line 263...
263 
 
 263 
 
264 
                debugOut.analog[12] = term[PITCH];
 264 
                debugOut.analog[12] = term[PITCH];
265 
                debugOut.analog[13] = term[ROLL];
 265 
                debugOut.analog[13] = term[ROLL];
266 
                debugOut.analog[14] = term[YAW];
 - 
 
267 
 
 - 
 
268 
                //DebugOut.Analog[18] = (10 * controlIntegrals[CONTROL_ELEVATOR]) / GYRO_DEG_FACTOR_PITCHROLL; // in 0.1 deg
 - 
 
269 
                //DebugOut.Analog[19] = (10 * controlIntegrals[CONTROL_AILERONS]) / GYRO_DEG_FACTOR_PITCHROLL; // in 0.1 deg
 - 
 
270 
                //debugOut.analog[22] = (10 * IPart[PITCH]) / GYRO_DEG_FACTOR; // in 0.1 deg
 - 
 
271 
                //debugOut.analog[23] = (10 * IPart[ROLL]) / GYRO_DEG_FACTOR; // in 0.1 deg
 266 
                debugOut.analog[14] = term[YAW];
272 
        }
 267 
        }