UAV Test Case- Insitu ScanEagle

This test case is based on the Unmanned Air Vehicle Systems 881C structure, weight distributions, and manufacturing complexities. All hardware objects are scaled to the weight of ScanEagle UAV. No changes are made to the software objects of the template. This example uses schedule dates of the ScanEagle program. No attempt has been made to simulate the ScanEagle design heritage or quantities of spares, prototypes, and production units. Therefore, this example should be viewed as an illustration of how the unmanned air vehicle systems template can be used to produce a rough cost estimate of a known UAV program.