Design and integration of electrical and hydraulic Control Systems to support equipment and facilities for ground test activities. Types of facilities to be engineered include component fatigue and static test machines, rotor and transmission test stands for performance and acceptance testing, power system test beds, airframe/landing gear drop test, airframe shake tests, aircraft tie-down facilities and flight test instrumentation. Responsibility spans from conceptual design to the operational product including resolution of all issues related to design, procurement, fabrication, installation and operation. In addition, the candidate may also be assigned to the oversight of the detail design and planning process as well as the support of subsequent documentation at the manufacturing, assembly and installation level. Candidate should have a familiarity with basic classical control system design concepts/methods and should have practical experience with electrical and electro-hydraulic motion control systems. The preferred candidate will possess a four-year degree in Electrical Engineering.