Hardware-in-the-Loop Test Platform for a Small Fixed Wing Unmanned Aerial Vehicle Embedded Controller

Onur B. Ertin, Halim Korkmaz, Ünver Kaynak, and Coşku Kasnakoğlu


UAV, hardware-in-the-loop simulation, HIL, autopilot, PID controller


Hardware-in-the-loop (HIL) test systems for unmanned aerial vehicles (UAV) embedded flight controllers provides more realistic test environments for pre-flight tests. The HIL test system which is described in this paper combines a detailed and sophisticated flight simulation software with a moving hardware platform in the pitch and roll axis with actual flight sensors to form a complete testing environment.

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