| dc.description.abstract | An air monitoring system (quadcopter) that have purposed to monitoring which
can control flying object through the air, have been designed. The quadcopter
system has a size of 30 cm x 30 cm which consists of four propellers (have length
20.32 cm). To maintaining of quadcopter during manufaring in the air, used
MMA7260Q accelerometer sensor. The remote control gives a command and the
receiver,it processed by the Atmega 328 microcontroller. The Atmega 328
microcontroller will read input data and signals on every component to execute
the command. Quadcopter using wireless cctv to recorded the object and was
equipped by a delivery system with RF433 transmitter. Then, data which have
been sent, is capture by receiver on PC. To connected the receiver with PC needed
a converter , it is needed because PC does not have AV connector (audio video),
so that, it would takes the easy capture. From the resulted and analyzed testing of
the motor, show that quadcopter response to elevated at pulse which started from
77 with have an average value of Revolution Per Minute (RPM) is 122.7 and
average value of Pulse Width Modulation (PWM) is 13.47 Hz. From the resulted
of slope testing, it was knew that the slope was depended by quadcopter position. | en_US |
