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Team: P15310 System Design Review Multi-Disciplinary Senior Design I Date: 10/02/2014 http://edge.rit.edu/edge/P15310/public/Problem%20Definition%20Documents

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* Matthew Partacz: Mechanical Engineer, Team Leader * Jameel Balenton: Electrical Engineer, Facilitator * Jeffrey Mayer: Electrical Engineer, Systems Engineer * James Carey: Computer Engineer, Website Administrator * Ricardo Quintanilla: Computer Engineer, Scribe * Leo Farnand: Faculty Guide MSD I - Team P15310 - Satcom on the Move 2

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3 * Problem Definition Recap * Functional Decomposition * Morph Chart * Concept Options/Models * Concept Selections * Feasibility Analysis * Concept Decisions * Fallback Plan * System Level Design Decisions * Functional Architecture * Draft Test Plan * Test Plan Risks * Project Plan * Questions, Comments, Suggestions.

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* Navigation Art of controlling and monitoring direction and position Before 1900: * Cross-Staff * Compass * Astrolabe * Chip Log * Hourglass * Quadrant * Sextant * Octant * Chronometer * Dead Reckoning After 1900: * Radio-beacon * LORAN * Transit Satellite Navigation * Radar * GPS * Inertial Navigation MSD I - Team P15310 - Satcom on the Move 4

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* Spectracom specializes in timing, related to navigation. * Precision timing and synchronization leads to global navigation and various communication technologies. * Global Positioning System (GPS) and an Inertial Measurement Unit (IMU) * Time, position, and attitude * Even in the case of a temporary GPS loss * Spectracom does not make higher level end products * Base to create any number of solutions Spectracoms Geo-PNT Module the project will focus on. MSD I - Team P15310 - Satcom on the Move 5

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* The Spectracom Geo-PNT product is a device capable of providing precise position, navigation, and timing. It is used for a variety of applications, but not limited to, unmanned autonomous systems (UAV), flight analyses, and communication networks. * Satcom-On-The-Move project will be a demonstration of Geo-PNTs primary features. * This will be performed by tracking a geosynchronous point during movement and testing the accuracy. * A three axis system will be created in order to conduct accuracy tests on the Geo-PNT product in addition to showing integration and simplicity. * This will be handled by providing visual and written test documentation, as well as a final marketing video. MSD I - Team P15310 - Satcom on the Move 7

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8 * A system capable of demonstrating pitch, roll, and yaw while maintaining closed-loop control. * Full written and video documentation of the system including a full drawing package. * Final summary and test report. * Promotional video demonstrating the system and the Geo-PNTs capabilities.

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MSD I - Team P15310 - Satcom on the Move 9 * Use a commercial TV satellite installed on an elevation over azimuth motorized mount attached to a vehicle. * This would offer a way to demonstrate the proper stable tracking of the satellite within a specified range of accuracy by the Geo-PNT. * The validation of the Geo-PNT is in proper reception of the TV signal without interruption throughout all motion of the vehicle. * Take Away Concept: Geo-PNT is navigated around and proven to maintain signal (or track the signal) from the satellite.

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MSD I - Team P15310 - Satcom on the Move 10 * Interface a camera with the Geo-PNT to track a specified object or target. * The camera, Geo-PNT, and transmitting antenna would be attached or mounted to a vehicle. * A video display will be setup at a remote location that will show a live feed of the camera view as it tracks the specified object. * Take Away Concept: This demonstrates the capabilities of the Geo-PNT, and offers a more economical solution in terms of equipment and feasibility.

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MSD I - Team P15310 - Satcom on the Move 12 General Dynamics X Band SATCOM on the Move DRS Technologies SATCOM on the move (2 Port Cross Pol Ku- Band) Rockwell Collins SWE-DISH SATCOM On-The-Move CCT Frequecy Recieving10.95 - 12.75 GHz10.70 - 12.75 GHz10.95 12.75 GHz Frequency Transmitting13.75 - 14.50 GHz13.75 - 14.5 GHz13.75 14.5 GHz Pedestal2 Axis Az/El360 Degree Azimuth Mount Tracking Performance FCC VMES Compliant (< 0.20 - 99% of the time during Churchville B conditions EI angle < 80)NA 0.1 RMS Size27.5" x 27.5" x 37.5"37.5 x 27.5 x 14.5 inches49" x 49" x 51" Supply Voltage28V NA Power336W cont, 1260W peak3000W peakNA Weight182 lbs60-85 lbs depending on options300 lbs

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MSD I - Team P15310 - Satcom on the Move 14 Customer Requirement Number ImportanceDescription CR019Demonstration of Geo-PNT System Accuracy CR029Demonstration of Geo-PNT Accuracy Loss over time during a fade CR033Video Report/Commercial (Visual Test Report) CR041Vehicle to provide movement of Geo-PNT CR059Demonstrate Full Range of motion of Geo-PNT CR069Closed Loop Control, based on Geo-PNT input CR071Complete documentation of how to operate the entire system CR089Complete documentation of system performance

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MSD I - Team P15310 - Satcom on the Move 15 Engineering Requirement Number ImportanceEngineering RequirementUnit of MeasureMarginal Value ER1.19Accuracy and minimum angular error of attitudes roll and pitch Degrees2.5 ER1.29Accuracy of attitude yawDegrees2.5 ER1.39Position accuracy error horizontalMeters1.5 ER1.49Position accuracy error verticalMeters2.5 ER1.59Position accuracy error velocityMeters/second1.5 ER2.19Accuracy of error over time of attitudes roll and pitch Degrees/hour3 ER2.29Accuracy of error over time of attitude yawDegrees/hour3 ER3.13Number of videos per demoNumber1 ER4.11Geo-PNT is mounted to a mobile objectMeters/second>0 ER5.19Motion in yawDegrees360 ER5.29Motion in pitch and rollDegrees180 ER6.19System functionality continues without user intervention N/AIndefinite ER7.13Provide a user manualN/AY/N ER8.13Provide a written and visual test reportN/AY/N

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