Wyle's approach to aircraft integration is based on a structured process applying the full range of our technical expertise and experience. System architectures are developed and hardware and software integration approaches are generated as a function of the detailed analysis of subsystem interface data. Wyle's cadre of subject matter experts ensures that interface specifications are generated and reviewed, interface hardware and software is developed and detailed system integration plans are established to facilitate the integration and testing process. Wyle's simulation and modeling tools are used to validate system interfaces in a controlled, structured laboratory environment prior to ground and flight test. This ordered test and validation method provides end-to-end system testing that is critical to early identification and resolution of problem areas.
Examples of Wyle’s Aeronautical Systems Integration work include:
Cooperative Engagement Capability (CEC) -- Wyle participated in the various modification programs designed to provide CEC for the E-2C, developing the specifications for the mission computer upgrade and for CEC integration into the E-2C aircraft. In addition to evaluating CEC hardware and software, Wyle generated procurement packages, provided inputs to the CEC/E-2C Test and Evaluation Master Plan and developing detailed test plans for CEC-E-2C integration testing.
Multifunctional Information Distribution (MIDS) -- Wyle played an integral role in the integration of the MIDS into the F/A-18C/D aircraft. Wyle generated inputs for the MIDS/F-18 TEMP, developed MIDS initialization parameters for F-18 installation, investigated test instrumentation requirements, developed data analysis tools to facilitate the analysis of test data, and participated in laboratory integration testing. Wyle also developed detailed ground and flight test procedures, including data analysis and data management procedures in support of the program.
E-2C Mini-DAMA -- Wyle was the primary support contractor to the E-2C/Mini-DAMA integration program. Wyle's efforts included evaluation of Mini-DAMA performance requirements, evaluation of aircraft-mounted SATCOM antennas, systems engineering and interface requirements analysis, and development of cost estimating relationships to predict test and evaluation and integration costs for SATCOM systems on Navy aircraft. Wyle also participated in laboratory integration testing of the installation of Mini-DAMA in the Hawkeye 2000 version of the E-2C, and an integral participant in both ground and flight testing.