Simulasi Hardware in the Loop Untuk Redundansi Tiga Modul Autopilot

Authors

  • M. Rasyid Al Ghafar Program Studi Teknik Elektro â?? STEI, Institut Teknologi Bandung, Bandung
  • Widyawardana Adiprawita School of Electric Engineering and Informatics Institut Teknologi Bandung

Abstract

Makalah ini menjelaskan tentang perancangan dan pengujian Hardware in the Loop (HIL) untuk tiga modul autopilot yang diredundansi. Redundansi autopilot merupakan upaya dalam mendesain suatu sistem yang tahan terhadap kegagalan pada sistem yang mungkin timbul pada pesawat udara, khususnya pesawat udara tanpa awak (UCAV). Pengujian HIL dilakukan dengan bantuan software X-Plane dan Qgroundcontrol, dimaksudkan untuk uji kelayakan autopilot sebelum di implementasikan pada perangkat atau pesawat sesungguhnya. Protokol komunikasi transfer data yang digunakan adalah UDP to serial dan serial to UDP yang dilakukan secara realtime. Dalam pengujian, modul redudansi autopilot telah berjalan dan terintegrasi dengan baik.

References

Koren, Israel et.al. 2007. Fault Tolerant Systems. Oxford: Elsevier, Inc.

Hitt, Eliss F. 2000. Digital Avionics Handbook, Second Edition. Boca Raton: CRC Press.

Fault Tolerance, http://www.cs.unc.edu/~anderson//teach/comp790/ papers/ fault_tolerance_avionics.pdf

Ardupilot, http://ardupilot.org/copter/docs/common-rfd900.html

Flight stack, http://px4.io/technology/px4-software-stack/

Pixhawk hardware, https://pixhawk.org/

3DR GPS, http://ardupilot.org/copter/docs/common-installing-3dr-ublox-gps-compass-module.html

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Published

2018-04-12

Issue

Vol. 1 No. 1 (2018)

Section

Articles

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