Web-Based Conversion of Correlated CGF Terrain Via SEDRIS

Not Available The proposed innovation is an autonomous device for verifying proper alignment between the launch bar of a Navy aircraft and the carrier-based catapult assembly. It is based on a robust, low cost mechanical position sensor and visual indicator located on the catapult spreader. In addition, a remotely located optical scanner detects the presence of the indicator and automatically prevents the catapult from firing until verification. The innovation addresses the stated subtopic requirements of eliminating the dangerous Hookup Petty Officer role, improving the reliability of the alignment observation, performing the verification with a wireless approach under all possible conditions, withstanding extreme force and acceleration, giving fast response, and having high durability. With the proposed approach, there are no modifications to the aircraft, nor are there electronics located on the catapult. In Phase I, we will develop the mechanical catapult sensor as well as the optical scanner. We will demonstrate the feasibility of making the verification reliably in extreme conditions. In Phase II, we will produce field deployable units for shipboard evaluation. The long distance identification hardware developed in this program has significant potential for commercial applications such as automated tollbooths, smart highways, high-speed manufacturing, freight transportation, and security systems.