MQ-8B Fire Scout UAV Manning Cost Benefit Analysis

EMBA Project ReportEXECUTIVE SUMMARY: At the request of the Intelligence, Surveillance, and Reconnaissance Task Force, the Naval Air Systems Command‘s program office for Multi-Mission Tactical Unmanned Aerial Systems (UAS)—also known as PMA-266, began MQ-8B flight operations in Afghanistan. Due to the importance and short notice of this request, the initial manning and support measures for the Fire Scout detachment has relied heavily on contractors. In an effort to refine and redirect the future manning of Fire Scout detachments, PMA-266 asked the Washington DC Naval Postgraduate School Consulting Group to evaluate three different courses of action (COAs) detailing manning options for deployment of the MQ-8B Fire Scout for the next year. The three COAs were: 1) Manning with a military component 2) Manning with NGC contract services 3) Manning through a third party contractor. This report recommends that PMA-266 use the military component COA to the maximum extent possible. In addition to annual cost savings of over $10M, a military component provides greater mission-focus and flexibility inherent in a military chain of command as compared to a contract manning structure. The Navy would also benefit by obtaining operational UAS experience as it looks to develop an unmanned aviation community. The experience gained could be used to develop Navy instructors for operator and maintenance training instead of continuing to rely on contract support for these requirements.For Capt Patrick Smith Director PMA-266http://archive.org/details/mqbfirescoutuavm10945707

Validation of the USNTPS simulator for the advanced flight controls design exercise

This thesis explores the fidelity of the ground based simulator used at USNTPS during the Advanced Flight Controls Design exercise. A Simulink model is developed as a test platform and used to compare the longitudinal flight characteristics of the simulator. The model is also compared to the same characteristics of a Learjet in the approach configuration. The Simulink model is modified with the aim of yielding a better training aid for the students as well as providing a means of comparison between the simulator flight data and the actual Learjet flight data. Open loop and closed loop trials are completed to gather data for analysis and improvement of the Simulink model. Regression analysis is also performed on the flight data as a means of comparing the longitudinal stability coefficients.http://archive.org/details/validationofusnt109451773Approved for public release; distribution is unlimited