Explain some reasons why “electo-optical” technology (glass) has merit in a helicopter. Balance this against the cost dynamics of new installation or retro fit to glass cockpits. Why go to “glass” if the missions are the same as before glass products? Are there any human factors that must be considered in such equipment transitions? Why is development of UAV rotorcraft vs fixed-wing UAVs such an important effort? What are some of the potential civil uses and concerns of a UAV?