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All Journal Mechatronics, Electrical Power, and Vehicular Technology JTERA (Jurnal Teknologi Rekayasa)
Egi Muhammad Idris Hidayat
Institut Teknologi Bandung
Civil Engineering, Building, Construction & Architecture Computer Science & IT Electrical & Electronics Engineering Industrial & Manufacturing Engineering Mechanical Engineering

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Design and implementation of hardware in the loop simulation for electric ducted fan rocket control system using 8-bit microcontroller and real-time open source middleware Yulnandi, Reza Aulia; Machbub, Carmadi; Prihatmanto, Ary Setijadi; Hidayat, Egi Muhammad Idris
Journal of Mechatronics, Electrical Power and Vehicular Technology Vol 8, No 1 (2017)
Publisher : Research Centre for Electrical Power and Mechatronics, Indonesian Istitutes of Sciences

Show Abstract | Download Original | Original Source | Check in Google Scholar | Full PDF (920.001 KB) | DOI: 10.14203/j.mev.2017.v8.60-69

Abstract

Hardware in the Loop Simulation (HILS) is intended to reduce time and development cost of control system design. HILS systems are mostly built by integrating both controller hardware and simulator software where the software is not an open source. Moreover, implementing HILS by using manufactured system is costly. This paper describes the design and implementation of HILS for Electric Ducted Fan (EDF) rocket by using open-source platform for development with middleware. This middleware system is used to bridge the data flow between controller hardware and simulator software. A low-cost ATMEGA 2560 8-bit microcontroller is used to calculate rocket’s attitude with Direction Cosine Matrix (DCM) algorithm and PID controller is employed to regulate rocket’s dynamics based on desired specifications. X-Plane 10 simulator software is used for generating simulated sensory data. The test results validate that HILS design meets the defined specifications, i.e. angle difference of 0.3 degrees and rise time of 0.149 seconds on pitch angle.
Design and implementation of hardware in the loop simulation for electric ducted fan rocket control system using 8-bit microcontroller and real-time open source middleware Reza Aulia Yulnandi; Carmadi Machbub; Ary Setijadi Prihatmanto; Egi Muhammad Idris Hidayat
Journal of Mechatronics, Electrical Power and Vehicular Technology Vol 8, No 1 (2017)
Publisher : National Research and Innovation Agency

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.14203/j.mev.2017.v8.60-69

Abstract

Hardware in the Loop Simulation (HILS) is intended to reduce time and development cost of control system design. HILS systems are mostly built by integrating both controller hardware and simulator software where the software is not an open source. Moreover, implementing HILS by using manufactured system is costly. This paper describes the design and implementation of HILS for Electric Ducted Fan (EDF) rocket by using open-source platform for development with middleware. This middleware system is used to bridge the data flow between controller hardware and simulator software. A low-cost ATMEGA 2560 8-bit microcontroller is used to calculate rocket’s attitude with Direction Cosine Matrix (DCM) algorithm and PID controller is employed to regulate rocket’s dynamics based on desired specifications. X-Plane 10 simulator software is used for generating simulated sensory data. The test results validate that HILS design meets the defined specifications, i.e. angle difference of 0.3 degrees and rise time of 0.149 seconds on pitch angle.
Perancangan Sistem Lokalisasi Sumber Suara Berdasarkan Metode TDOA dan DTOF Resti Fauziah; Carmadi Machbub; Egi Muhammad Idris Hidayat
JTERA (Jurnal Teknologi Rekayasa) Vol 5, No 2: December 2020
Publisher : Politeknik Sukabumi

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.31544/jtera.v5.i2.2020.295-302

Abstract

Pada penelitian ini dibahas perancangan sistem lokalisasi sumber suara dengan menggunakan metode Time Difference of Arrival (TDOA) dan metode Difference of Time of Flight (DTOF). TDOA merupakan metode penentuan posisi sumber suara berdasarkan pada persamaan hiperbola pada bidang koordinat dan hubungan selisih titik fokus hiperbola dari sinyal-sinyal yang diperoleh pada beberapa sensor berupa mikrofon dengan waktu kedatangan yang menggunakan waktu mutlak tiba di mikrofon tertentu. DTOF merupakan metode penentuan posisi sumber suara yang diturunkan berdasarkan perbedaan waktu propagasi sinyal dari sumber suara ke setiap mikrofon saat mikrofon dipicu. Sebagai pembuktiannya dilakukan dengan dua cara. Pertama, simulasi dengan waktu setiap mikrofon ialah jarak mikrofon terhadap sumber suara dibagi dengan kecepatan suara. Kedua, eksperimen dengan waktu setiap mikrofon ialah hasil rekaman suara yang waktu tundanya diperoleh dengan membandingkan Korelasi Silang dan Korelasi Silang Umum. Berdasarkan simulasi dan eksperimen dapat disimpulkan bahwa metode TDOA menghasilkan akurasi yang lebih baik.
Co-Authors Ary Setijadi Prihatmanto Carmadi Machbub Resti Fauziah Reza Aulia Yulnandi Yulnandi, Reza Aulia