Flight control system merupakan suatu sistem di pesawat udara yang digunakan untuk pergerakan pesawat di udara dari satu kondisi terbang ke kondisi terbang lainnya. Alat uji flight control system actuator pesawat ini untuk mengetahui beban yang diterima terhadap jarak dari pergerakan aktuator pesawat. Sistem akuisisi data dari alat uji flight control actuator berupa data beban dan jarak, serta pemberian PWM (Pulse Width Modulation). Data akuisisi menggunakan
bantuan software Labview sebagai software untuk memprogram dan interface data akuisisi pada PC dan juga pada bagian hardware mekanikal menggunakan mikrokontroler arduino uno sebagai media untuk akuisisi data. DAQ alat uji flight control actuator pesawat dirancang menggunakan LabView yang telah direalisasikan, yaitu mampu menampilkan data berat yang diterima aktuator, yang berupa motor servo sebagai unit under test, dengan berat maksimum 2
kg serta mampu menampilkan data pergerakan unit under test dari pergerakan 3 cm – 5 cm, serta mampu menampilkan PWM yang diberikan pada unit under test saat bergerak maju sebesar 45, saat bergerak mundur 135 dan saat berhenti 90.
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