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Contact Name
Dewi Muliyati
Contact Email
dmuliyati@unj.ac.id
Phone
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Journal Mail Official
snf@unj.ac.id
Editorial Address
Fisika FMIPA Universitas Negeri Jakarta GHA Lt.5 Jl Rawamangun Muka No.1
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Kota adm. jakarta timur,
Dki jakarta
INDONESIA
PROSIDING SEMINAR NASIONAL FISIKA (E-JOURNAL)
ISSN : 23021829     EISSN : 24769398     DOI : https://doi.org/10.21009/03
Focus and Scope: Physics education Physics Instrumentation and Computation Material Physics Medical Physics and Biophysics Physics of Earth and Space Physics Theory, Particle, and Nuclear Environmental Physics and Renewable Energy
Articles 976 Documents
KALIBRASI SEISMOMETER BBVS-120:G05402VS DENGAN METODE KOMPARASI B. Simbolon; M. Delina; B. Heryanto
PROSIDING SEMINAR NASIONAL FISIKA (E-JOURNAL) Vol 5 (2016): PROSIDING SEMINAR NASIONAL FISIKA (E-JOURNAL) SNF2016
Publisher : Program Studi Pendidikan Fisika dan Program Studi Fisika Universitas Negeri Jakarta, LPPM Universitas Negeri Jakarta, HFI Jakarta, HFI

Show Abstract | Download Original | Original Source | Check in Google Scholar | Full PDF (494.49 KB) | DOI: 10.21009/0305020122

Abstract

Calibration has been performed SeismometerBBVS-120: G05402VS in Calibration Laboratory Meteorology and Geophysics Kemayoran. Seismometer calibration performed with comparative method which compares the seismometers are calibrated with similar seismometer. Seismometers placed parallel and adjacent to each other (± 10 cm) so that the movement of the land received by the seismometer is the same. Comparison data were processed using software comparison . As a result, a new sensitivity values obtained with the acquisition value of the sensitivity seismometer Horizontal EW 2142 V / m / s, Horizontal NS 2096 V / m / s and Vertical UD 2137 V / m / s. Based on the manufacturer's specifications, the seismometer BBVS-120: G05402VS had a sensitivity of 2000 V / m / s. In overall results of this calibration is still in both categories. Keywords: calibration, comparison, sensitivity.
SISTEM KENDALI SUHU DAN PEMANTAUAN KELEMBABAN UDARA RUANGAN BERBASIS ARDUINO UNO DENGAN MENGGUNAKAN SENSOR DHT22 DAN PASSIVE INFRARED (PIR) Hannif Izzatul Islam; Nida Nabilah; Sofyan Sa'id Atsaurry; Dendy Handy Saputra; Gagat Mughni Pradipta; Ade Kurniawan; Heriyanto Syafutra; Irmansyah Irmansyah; Irzaman Irzaman
PROSIDING SEMINAR NASIONAL FISIKA (E-JOURNAL) Vol 5 (2016): PROSIDING SEMINAR NASIONAL FISIKA (E-JOURNAL) SNF2016
Publisher : Program Studi Pendidikan Fisika dan Program Studi Fisika Universitas Negeri Jakarta, LPPM Universitas Negeri Jakarta, HFI Jakarta, HFI

Show Abstract | Download Original | Original Source | Check in Google Scholar | Full PDF (989.029 KB) | DOI: 10.21009/0305020123

Abstract

We have been successfully to create a Control System Temperature and Air Humidy Monitoring Room Based on Arduino Uno with DHT22 Sensor and Passive Infrared (PIR). DHT22 Sensor be used as a measurement of temperature and air humidity in the room and Passive Infrared Sensor as a tool of detection the movement of people in a room. In this experiment, carried out tests of the DHT22 sensor and digital thermometer with a type AZ-HT-02 to room temperature with a hot air given through a hairdryer for 3 minutes with a span of per 10 seconds. In this test, the obtained data is that the room temperature is which measured by DHT22 sensor have an average difference of 0.93 against digital thermometer (as a calibration). In this test also obtained DHT22 sensor more sensitive Rrelative Humidity (RH), this is caused when given the hot air, humidity measured more rapid adjustment and yet different with digital temperature was slow to adjust air humidity in the room. This device using an Arduino Uno board, a Liquid Crystal Display (LCD) module and Real Time Clock (RTC) as a display of the temperature and air humidity in real time. This device is connected to a fan that can stabilize the room temperature are considered less convient to do activities in the room. Keywords: Air Humidity, Arduino Uno, DHT22 Sensor, Passive Infrared Sensor, Temperature.
SOLUSI PERSAMAAN DIFUSIVITAS ALIRAN FLUIDA MINYAK PADA RESERVOIR DAN MODIFIKASINYA UNTUK UJI ALIR (PRESSURE DRAWDOWN TEST) DAN UJI TUTUP (PRESSURE BUILDUP TEST) Hardiyanto Hardiyanto; Lilik Hendrajaya
PROSIDING SEMINAR NASIONAL FISIKA (E-JOURNAL) Vol 5 (2016): PROSIDING SEMINAR NASIONAL FISIKA (E-JOURNAL) SNF2016
Publisher : Program Studi Pendidikan Fisika dan Program Studi Fisika Universitas Negeri Jakarta, LPPM Universitas Negeri Jakarta, HFI Jakarta, HFI

Show Abstract | Download Original | Original Source | Check in Google Scholar | Full PDF (706.92 KB) | DOI: 10.21009/0305020124

Abstract

Pressure transient of oil in reservoir can be obtained from the solution diffusivity equation. To find a solution of this diffusivity equation takes two boundary conditions as space dimension and one dimension of the initial state as a condition for the time dimension. The solution is determined by using the Laplace transform and then used as a test analysis of pressure drop in a flow test (Pressure Drawdown Test) and Pressure buildup Test. The plot of the solution used to prediction reservoir parameters such as permeability, skin faktor , volume of the reservoir, Dietz Shape faktor and the average pressure. Keywords: diffusion equation, the pressure transient, the drawdown-buildup.
RANCANG BANGUN DAN KENDALI SEMI-OTOMATIS HEXACOPTER DENGAN ALGORITMA GENETIK A* Lanny Catrin Dale; Surya Darma; Prawito Prawito
PROSIDING SEMINAR NASIONAL FISIKA (E-JOURNAL) Vol 5 (2016): PROSIDING SEMINAR NASIONAL FISIKA (E-JOURNAL) SNF2016
Publisher : Program Studi Pendidikan Fisika dan Program Studi Fisika Universitas Negeri Jakarta, LPPM Universitas Negeri Jakarta, HFI Jakarta, HFI

Show Abstract | Download Original | Original Source | Check in Google Scholar | Full PDF (1037.527 KB) | DOI: 10.21009/0305020125

Abstract

This paper reports Hexacopter Design (drone) with a single parameter power lift drone. Target maximum load adjusted to the motor and propeller selection of components to be used. On the other hand, Hexacopter utilizing Genetic Algorithm type A* aims to determine the shortest path is most likely, from a start position to a final desired location. Some obstacles will be registered on the color histogram algorithm as a detection technique, then A* will utilize the position of the obstacles to recalculate the most optimal path so that another drone move without bumping into obstacles. Movement control drone utilizing proportional, integral and differential simple known as PID. The determination of the constants in the PID control drone applications utilize auto-tuning of the mission planner. Experiments conducted in a room with virtual grids which share the track from the starting point to the destination location. The obstacles placed in the position of 1.5 meters above the floor so that the image processing is projected to virtual grids. The position of the projected results become inputs A* to calculate the trajectory. The next stage of testing will also be done on the outside of the building space with the use of GPS in lieu of the grid in question. The results of this study reported how the drones will act with the implementation of the intelligence to control a semi-automatic movement. Keywords: Design , Hexacopter , Genetic Algorithm A* , the shortest path and control hexacopter .
PEMBUATAN ALAT SPIN COATER BERKECEPATAN SUDUT TINGGI BERBASIS ARDUINO UNO Sofyan Sa'id Atsaurry; Hannif Izzatul Islam; Nida Nabilah; Dendy Handy Saputra; Gagat Mughni Pradipta; Ade Kurniawan; Heriyanto Syafutra; Ardian Arif; Irzaman Irzaman
PROSIDING SEMINAR NASIONAL FISIKA (E-JOURNAL) Vol 5 (2016): PROSIDING SEMINAR NASIONAL FISIKA (E-JOURNAL) SNF2016
Publisher : Program Studi Pendidikan Fisika dan Program Studi Fisika Universitas Negeri Jakarta, LPPM Universitas Negeri Jakarta, HFI Jakarta, HFI

Show Abstract | Download Original | Original Source | Check in Google Scholar | Full PDF (450.962 KB) | DOI: 10.21009/0305020126

Abstract

We have managed to create a high corner velocity spin coater based Arduino Uno. This device assisted with brushless motor and infrared sensor as detection of brushless motor rotation. In experiment conducted research corner velocity of brushless motor on input value 1000 rpm, 2000 rpm, 3000 rpm, 4000 rpm, 5000 rpm, 6000 rpm, 7000 rpm, 8000 rpm, 9000 rpm, 10000 rpm, 11000 rpm, 12000 rpm, 13000 rpm, 14000 rpm, 15000 rpm,16000 rpm, 17000 rpm, 18000 rpm, 19000 rpm, and 20000 rpm on spin coater. In this research data showed that the corner velocity that measured by spin coater has difference average is 82.67 rpm with tachometer. Keywords: Arduino, Microcontroller, Brushless Motor, PID, Spin Coating.
RANCANG BAGUN ALAT GEOLISTRIK BERBASIS PULSE –WIDTH MODULATION (PWM) Akbar Muhammad; Handayani Gunawan
PROSIDING SEMINAR NASIONAL FISIKA (E-JOURNAL) Vol 5 (2016): PROSIDING SEMINAR NASIONAL FISIKA (E-JOURNAL) SNF2016
Publisher : Program Studi Pendidikan Fisika dan Program Studi Fisika Universitas Negeri Jakarta, LPPM Universitas Negeri Jakarta, HFI Jakarta, HFI

Show Abstract | Download Original | Original Source | Check in Google Scholar | Full PDF (1115.375 KB) | DOI: 10.21009/0305020127

Abstract

Kebutuhan alat survai geofisika sangat tinggi, terutama alat geolistrik. Tinggi kebutuhan tersebut membuat alat geolistrik menjadi sangat mahal. Untuk memecahkan masalah tersebut, maka muncul ide pembuatan geolistrik. Alat geolistrik adalah suatu alat geofisika untuk mengetahui aliran arus listrik kedalam tanah. Alat geolistrik menginjeksikan arus listrik tegangan DC. Kemudian di dalam tanah akan meimbulkan bedapotensial, bedapotensial tersebut kemudian diukur memgunakan voltmeter. Pada pembuatan geolistrik dimana tengangan DC yang diperoleh dari power supplay. Power supplay yang digunakan berbasis PWM (pulse-width modulation). Prinsip dasar dari PWM adalah menaikan tegangan DC dengan teknik modulasi. Teknik PWN banyak digunakan sebagai penguat amplifier karena memberikan tegangan DC dan arus DC yang cukup besar. Pengunaan PWM tersebut kemudian diubah menjadi power supllay geolistrik karena alat geolistrik memerlukan tegangan DC yang cukup besar untuk memijeksi arus ke dalam tanah pada bentangan yang cukup panjang. Kata-kata kunci: Geolistrik, Power Supplay, PWM, Tegangan DC.
STUDI PENGARUH SCREEN MESH TERHADAP INTENSITAS TURBULENSI PADA TEROWONGAN ANGIN SIRKUIT TERBUKA Nurul Mahilda; Cecep E Rustana; Umiatin Umiatin
PROSIDING SEMINAR NASIONAL FISIKA (E-JOURNAL) Vol 5 (2016): PROSIDING SEMINAR NASIONAL FISIKA (E-JOURNAL) SNF2016
Publisher : Program Studi Pendidikan Fisika dan Program Studi Fisika Universitas Negeri Jakarta, LPPM Universitas Negeri Jakarta, HFI Jakarta, HFI

Show Abstract | Download Original | Original Source | Check in Google Scholar | Full PDF (568.168 KB) | DOI: 10.21009/0305020128

Abstract

Screen Mesh is a filter made of wire that serves to remove the fine vortex structure by equating the speed variation of wind flow in the wind tunnel. Adding the screen mesh is to determine the effect of screen mesh to the value of turbulence intensity on open circuit wind tunnel. In this study, it has been made three pieces of screen mesh with each diameter of 46.5 cm, 48.5 cm and 50.5 cm. The tests was carried out by using screen mesh with rhombic mesh with 3 mm diagonal length that placed on X/L 0.67, 0.8, and 0.93. This research was conducted by comparing the results of turbulence intensity measurements between the wind tunnel without screen mesh, wind tunnel with honeycomb and screen mesh, as well as wind tunnel with only screen mesh so that we can know the flow quality in the wind tunnel. The test results indicated that the screen mesh has the ability to minimize the turbulence intensity. The wind tunnel that is installed using a honeycomb cell has 6 mm diameter and the 3 pieces of screen mesh has the lowest turbulence intensity that is I ≈ 0,0242. Keywords: wind tunnel, screen mesh, turbulence intensity.
PEMODELAN DAN SIMULASI TOPOLOGI SINGLE ENDED PRIMARY INDUCTOR CONVERTER (SEPIC) UNTUK MINI 3 PLUS WIND TURBINE Ryan Prasetiyo; Dwindra Wilham Maulana; Camellia Panatarani; I Made Joni
PROSIDING SEMINAR NASIONAL FISIKA (E-JOURNAL) Vol 5 (2016): PROSIDING SEMINAR NASIONAL FISIKA (E-JOURNAL) SNF2016
Publisher : Program Studi Pendidikan Fisika dan Program Studi Fisika Universitas Negeri Jakarta, LPPM Universitas Negeri Jakarta, HFI Jakarta, HFI

Show Abstract | Download Original | Original Source | Check in Google Scholar | Full PDF (801.285 KB) | DOI: 10.21009/0305020129

Abstract

In order to have a DC-DC buck boost converter with performances as desired specifications, the design process was performed by developing a model and simulation. The purpose of this research was to design a converter applied for a MINI 3 plus Wind Turbine. The converter topology was designed with Single Ended Primary Inductor Converter (SEPIC) using a Continuous Conduction Mode (CCM). The output specifications of converter are input voltage 60 V, input current 7,5 A, output voltage 25 V, output current 4,17 A, and frequency 25kHz. The average state space method was used to obtain its transfer function. The transfer function represented the characteristics of an average state of SEPIC converter system. The characteristics and designed quality of SEPIC converter determined by system performance analysis. The results showed that as designed SEPIC converter achieved excellent performances and stability based on their overshoot, rise time, settling time, frequency, and location of pole-zeros. Incontrast, the designed SEPIC converter showed that converter increased the input voltage (boost mode) with duty cycle more than 50% and reduced voltage (buck mode) with duty cycle less than 50%. It was concluded that the designed converter system achieved excellent and stable performances. Keywords: SEPIC converter, state space analysis, transfer function, DC-DC converter.
PENGUKURAN DAN ANALISA DATA KALIBRASI VOLTMETER DENGAN MULTI PRODUCT CALIBRATOR R. Uli; M. Delina; B. Heryanto
PROSIDING SEMINAR NASIONAL FISIKA (E-JOURNAL) Vol 5 (2016): PROSIDING SEMINAR NASIONAL FISIKA (E-JOURNAL) SNF2016
Publisher : Program Studi Pendidikan Fisika dan Program Studi Fisika Universitas Negeri Jakarta, LPPM Universitas Negeri Jakarta, HFI Jakarta, HFI

Show Abstract | Download Original | Original Source | Check in Google Scholar | Full PDF (666.874 KB) | DOI: 10.21009/0305020130

Abstract

To obtain a stable electrical voltage measurements and valid, voltmeter should undergo periodic calibration with Multi Product Calibrator traceable to National Standards or International Standards. Calibration measurements performed in the DC and AC parameters on each test points ranging from the smallest to largest according to ability voltmeter. For AC voltage used in the calibration frequency setting 50Hz and 10kHz. Analysis of calibration measurements are looking for is a correction value voltmeter with Multi Product Calibrator and uncertainty (uncertainty) at each test point. The results obtained calibration Digital Multimeter 29990020 series for DC voltmeter, at least 100mV test points as correction value and its uncertainty are (-2,98x10-3) mV and ± 0,011mv, while the biggest points 250V test correction value and its uncertainty is (-0 , 0229) V and ± 0,0667V. And for AC voltmeter at the test points 10mV 50Hz smallest correction value and its uncertainty are (1,3x10-3) mV and ± 0,037mv, while at 10kHz frequency correction value and its uncertainty are (-9.9929) mV and ± 0, 0685V. For AC voltmeter at the test points 220V, 50Hz largest correction value and its uncertainty is (-0,41) V and ± 0,245V, sedangkkan at 10kHz frequency correction value and its uncertainty are (-0,235) V and ± 1,088V. Based on this calculation, it was concluded that the voltmeter still unfit for use and valid for a tiny correction value below 1V. Key words: calibration voltmeter, Multi-Product Calibrator, uncertainty of measurement.
ANOMALI MEDAN GRAVITASI PERMUKAAN (G) AKIBAT GERHANA MATAHARI SEBAGIAN (GMS) 9 MARET 2016 MENGGUNAKAN ANALISIS TRACKER PADA KATER’S REVERSIBLE PENDULUM Fitri Nurul Sholihat; Suci Ramayanti; Anggi Hanif Setyadin; Ardi Rizkia Ferahenki; Muhamad Gina Nugraha; Duden Saepuzaman; Achmad Samsudin; Judhistira Aria Utama; Hana Susanti; Kartika Hajar Kirana
PROSIDING SEMINAR NASIONAL FISIKA (E-JOURNAL) Vol 5 (2016): PROSIDING SEMINAR NASIONAL FISIKA (E-JOURNAL) SNF2016
Publisher : Program Studi Pendidikan Fisika dan Program Studi Fisika Universitas Negeri Jakarta, LPPM Universitas Negeri Jakarta, HFI Jakarta, HFI

Show Abstract | Download Original | Original Source | Check in Google Scholar | Full PDF (691.814 KB) | DOI: 10.21009/0305020131

Abstract

This study was conducted to determine the gravitational field of the Earth's surface anomaly (g) due to the partial solar eclipse. Large gravity field of Earth's surface can be obtained using a pendulum swing period. Data were collected for three days on 8, 9, and 10 March, 2016 from at 6:00 to 9:00 pm in Bandung with coordinates 6°51'48 " LS, 107°35'40" BT. The tools used in this research was Kater's reversible pendulum with a deviation of less than 3° so that the motion can be regarded swing harmonics. Pendulum swinging motion is recorded using high resolution cameras (High definition) with a shooting speed 24 of frames per second (fps), the video is analyzed using the tracker in order to obtain the period of a pendulum swing. The results show the value of the gravitational field of the Earth's surface on a three-day consecutive sampling of 10,33153834, 10,18560435, and 10,32046468. According to the research there are anomalies in the gravitational field of the Earth's surface (g) due to the partial solar eclipse with the value of the gravitational field which decreases the time of the eclipse. Keywords: Eclipse, Tracker, Kater’s Reversible Pendulum.

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