Development of User Interface Based on LabVIEW for Unmanned Aircraft Application

Authors

  • Faaris Mujaahid Universitas Muhammadiyah Yogyakarta
  • Amir Malik Hizbullah Universitas Muhammadiyah Yogyakarta
  • Febrian Dhimas Syahfitra Universitas Muhammadiyah Yogyakarta
  • Muhammad Abduh Dahlan Universitas Muhammadiyah Yogyakarta
  • Nugroho Dwi Juliansyah Universitas Muhammadiyah Yogyakarta

DOI:

https://doi.org/10.18196/jet.1214

Keywords:

User Interface, Condition monitoring, LabVIEW, Rocket

Abstract

This paper describes the user interface construction of rocket/aircraft condition monitoring systems on LabVIEW, a graphical-based programming language. The interface, placed in the ground station, has some important information transmitted from the rocket. The information contains real-time data from the sensor devices. The aim of the construction of this interface is that the operator in the ground station can monitor the behavior and the condition of the flying rocket, in regard to the self-control mechanism programmed within the rocket. The LabVIEW front panel includes the visualization of 3D rocket motion, accelerometer-graph, gyroscope-graph, rocket navigation, GPS positioning, altitude, and pressure-meter. The result proved that the data transmission was recorded properly to the front panel system and logbook. In addition to the result, the reliability test has 50% probability to the system performance with the given test period of 300 seconds and 600 seconds. The low reliability result might be caused by the size of buffer overflow between the hardware and LabVIEW.

Author Biographies

Faaris Mujaahid, Universitas Muhammadiyah Yogyakarta

Department of Electrical Engineering

Amir Malik Hizbullah, Universitas Muhammadiyah Yogyakarta

Department of Electrical Engineering

Febrian Dhimas Syahfitra, Universitas Muhammadiyah Yogyakarta

Department of Electrical Engineering

Muhammad Abduh Dahlan, Universitas Muhammadiyah Yogyakarta

Department of Electrical Engineering

Nugroho Dwi Juliansyah, Universitas Muhammadiyah Yogyakarta

Department of Electrical Engineering

References

Zhang, Y., Wu, J., Huang, M., Zhu, H., Chen, Q. (1998). Liquid-Propellant Rocket Engine Health-Monitoring Techniques. Journal of Propulsion and Power. 14 (5). 657-663.

Wiyagi, R. O., Danardono, Agus, T. A. (2017). High Altitude Balloon Payload Design for Atmospheric Observations. Journal of Electrical Technology UMY (JET-UMY), 1(1). 50-57.

LAPAN. (2015). Komurindo dan Kombat 2015 Sukses Dilaksanakan. LAPAN, Deputy of Space Science and Atmosphere. Access date: 21 June 2017.

Jimenez, C., Faerevaag, C. L., Jentsch, F. (2016). User Interface Design Recommendation for Small Unmanned Aircraft Systems (sUAS). International Journal of Aviation, Aeronautics, and Aerospace. 3 (2).

Sudesh, M. (2013). An Unmanned Air Vehicle Simulator in C#, M.Sc. theses, Dept. Computer Science, North Dakota State University of Agriculture and Applied Science, North Dakota.

Kalra, A., Anand, P., Singh, S. (2014). Flight Simulation Using Graphical User Interface. Advances in Aerospace Science and Applications. 4 (1). 85-90.

HobbyKing. Dr. Mad Thrust 90mm Blade Alloy EDF 1400kv – 2500w (6S). Access date: 10 July 2017.

National Instruments. Advantages of LabVIEW in Academic Research. Access date: 10 July 2017.

Tasner, T., Lovrec, D., Tasner, F., Edler, E. (2012). Comparison of LabVIEW and MATLAB for Scientific Research. Annals of Faculty Engineering Hunedoara - International Journal of Engineering. 389-394.

National Instruments. (2013). Getting Started with LabVIEW. Access date: 10 July 2017.

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Published

2017-06-30

How to Cite

Mujaahid, F., Hizbullah, A. M., Syahfitra, F. D., Dahlan, M. A., & Juliansyah, N. D. (2017). Development of User Interface Based on LabVIEW for Unmanned Aircraft Application. Journal of Electrical Technology UMY, 1(2), 106–111. https://doi.org/10.18196/jet.1214

Issue

Section

Articles