This document describes the design of a flight stabilization system for an unmanned aerial vehicle (UAV) using hardware-in-the-loop (HIL) testing. Controllers were designed separately for longitudinal and lateral flight axes using simulations. The controllers successfully stabilized straight and level flight in HIL tests. The document discusses the aircraft dynamics, controller designs for elevators and ailerons, multivariable control system design, and HIL test platform used to validate the controllers.