ANALISIS AVIONIC SYSTEM PESAWAT UAV PUNA AD-01

RIZKI SEPTIAN, ARI (2019) ANALISIS AVIONIC SYSTEM PESAWAT UAV PUNA AD-01. Skripsi thesis, Institut Teknologi Dirgantara Adisutjipto.

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Abstract

Aircraft without crew or PUNA is aircraft that fly without a crew, PUNA can be controlled using remote or autonomous flying depends on aircraft specifications. PUNA has been widely circulating in the market and has been widely used for reconnaissance and monitoring missions in the area or region. PUNA AD-01 using 8000 mAh battery can perform the endurance calculations based on flight tests. In the analysis of the Avionic System PUNA AD-01, it used analytical and testing methods. Avionic understanding is an electronic system that is applied to aircraft which is useful to facilitate the aircraft while flying. Avionic in aircraft related to the power supply of each component which flowed electric current obtained from the battery. Through the process of propulsion testing and flight testing, it is use to get the value of the battery current and voltage as an endurance calculation. The results of propulsion testing data using propulsion test equipment on the maximum power of brushless motors are known the average. of the voltage which is 13-14 volts while for the current value at maximum power is obtained with an average value of 25 A. while the flight test analysis and Ardupilot simulation data use PUNA AD-01 aircraft mission planner is known to be current at cruising with an average value of 12 A and 38-39 minutes of endurance is obtained using an 8000 mAh battery.

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