The physical Zagi HP Electric Flying Wing RC Aircraft, only utilized the successive loop closure control design method. The physical system performed similar to the successive loop closure simulation results – it was able to track altitude commands with more desirable response characteristics than that of course heading commands.

Figure 16 below shows several images of the completed Zagi HP Electric Flying Wing RC Aircraft used as the physical system throughout the project.

Figure 16: Zagi HP Electric Flying Wing RC Aircraft Physical System from [6]