Rancangan Quadcopter Untuk Sistem Pemantau Udara Berbasis Mikrokontroller ATmega 328
RANCANGAN QUADCOPTER UNTUK SISTEM PEMANTAU
UDARA BERBASIS MIKROKONTROLLER ATMEGA 328
ABSTRAK
Telah dirancang sebuah sistem pemantau udara (quadcopter ) untuk pemantau
yang dapat mengendalikan objek terbang di udara. Sistem quadcopter tersebut
memiliki ukuran 30 cm x 30 cm terdiri dari empat buah baling baling (panjang
20.32 cm). Dalam menjaga keseimbangan quadcopter selama bermanufare di
udara, digunakan sensor accelerometer MMA7260Q. Remote control memberikan
perintah dan ditangkap receiver pada quadcopter , perintah atau data yang diterima
oleh receiver diproses oleh mikrokontroller ATmega 328. ATmega 328 membaca
data yang diberikan dan memberikan sinyal pada setiap komponen untuk
melaksanakan perintah. Quadcopter menggunakan cctv wireless yang dapat
merekam objek dan dilengkapi dengan sistem pengiriman dengan pemancar
Rf433. Kemudian data yang dikirim ditangkap oleh receiver pada PC. Untuk
menghubungkan antara penerima (receiver ) dengan Personal Computer (PC)
dibutuhkan converter , hal ini dibutuhkan karena pada Personal Computer (PC)
tidak mempunyai konektor AV (audio video), oleh sebab itu dibutuhkan easy
capture . Dari hasil pengujian motor, quadcopter mendapatkan respon untuk
terangkat dimulai dari pulsa 77 dengan rata-rata nilai Revolution Per
Minute (RPM) 122.75 dan rata-rata Pulse Width Modulation (PWM) 13.47 Hz.
Dari hasil pengujian kemiringan dapat diketahui bahwa kemiringan tergantung
posisi quadcopter.
Kata Kunci : Quadcopter , Sensor accelerometer MMA7260Q, Mikrokontroller
ATmega 328, PC, baling-baling.
v
Universitas Sumatera Utara
DESIGNING OF QUADCOPTER FOR AIR MONITORING
SYSTEM BASED WITH ATMEGA 328 MICROCONTROLLER
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.
Keywords: Quadcopter, MMA7260Q accelerometer sensor, Microcontroller
ATmega 328, PC, Propeller.
vi
Universitas Sumatera Utara
UDARA BERBASIS MIKROKONTROLLER ATMEGA 328
ABSTRAK
Telah dirancang sebuah sistem pemantau udara (quadcopter ) untuk pemantau
yang dapat mengendalikan objek terbang di udara. Sistem quadcopter tersebut
memiliki ukuran 30 cm x 30 cm terdiri dari empat buah baling baling (panjang
20.32 cm). Dalam menjaga keseimbangan quadcopter selama bermanufare di
udara, digunakan sensor accelerometer MMA7260Q. Remote control memberikan
perintah dan ditangkap receiver pada quadcopter , perintah atau data yang diterima
oleh receiver diproses oleh mikrokontroller ATmega 328. ATmega 328 membaca
data yang diberikan dan memberikan sinyal pada setiap komponen untuk
melaksanakan perintah. Quadcopter menggunakan cctv wireless yang dapat
merekam objek dan dilengkapi dengan sistem pengiriman dengan pemancar
Rf433. Kemudian data yang dikirim ditangkap oleh receiver pada PC. Untuk
menghubungkan antara penerima (receiver ) dengan Personal Computer (PC)
dibutuhkan converter , hal ini dibutuhkan karena pada Personal Computer (PC)
tidak mempunyai konektor AV (audio video), oleh sebab itu dibutuhkan easy
capture . Dari hasil pengujian motor, quadcopter mendapatkan respon untuk
terangkat dimulai dari pulsa 77 dengan rata-rata nilai Revolution Per
Minute (RPM) 122.75 dan rata-rata Pulse Width Modulation (PWM) 13.47 Hz.
Dari hasil pengujian kemiringan dapat diketahui bahwa kemiringan tergantung
posisi quadcopter.
Kata Kunci : Quadcopter , Sensor accelerometer MMA7260Q, Mikrokontroller
ATmega 328, PC, baling-baling.
v
Universitas Sumatera Utara
DESIGNING OF QUADCOPTER FOR AIR MONITORING
SYSTEM BASED WITH ATMEGA 328 MICROCONTROLLER
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.
Keywords: Quadcopter, MMA7260Q accelerometer sensor, Microcontroller
ATmega 328, PC, Propeller.
vi
Universitas Sumatera Utara