Team P 15310 System Design Review MultiDisciplinary Senior

Team: P 15310 System Design Review Multi-Disciplinary Senior Design I Date: 10/02/2014 http: //edge. rit. edu/edge/P 15310/public/Problem%20 Definition%20 Documents In cooperation with…

* * Matthew Partacz: Mechanical Engineer, Team Leader *Jameel Balenton: Electrical Engineer, Facilitator *Jeffrey Mayer: Electrical Engineer, Systems Integrator *James Carey: Computer Engineer, Website Administrator *Ricardo Quintanilla: Computer Engineer, Scribe *Leo Farnand: Faculty Guide MSD I - Team P 15310 - Satcom on the Move 2

* * 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. MSD I - Team P 15310 - Satcom on the Move 3

* * Navigation – Art of controlling and monitoring direction and position Before 1900: After 1900: * Cross-Staff * Compass * Astrolabe * Chip Log * Hourglass * Quadrant * Sextant * Octant * Chronometer * Dead Reckoning MSD I - Team P 15310 - Satcom on the Move * Radio-beacon * LORAN * Transit Satellite Navigation * Radar * GPS * Inertial Navigation 4

* *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 Spectracom’s Geo-PNT Module the project will focus on. MSD I - Team P 15310 - 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-PNT’s 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 P 15310 - Satcom on the Move 7

* *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-PNT’s capabilities. MSD I - Team P 15310 - Satcom on the Move 8

* * 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. MSD I - Team P 15310 - Satcom on the Move 9

* * 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. MSD I - Team P 15310 - Satcom on the Move 10

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* DRS Technologies SATCOM on General Dynamics X Band SATCOM on the move (2 Port Cross Pol Ku- Rockwell Collins SWE-DISH Move Band) SATCOM On-The-Move CCT Frequecy Recieving 10. 95 - 12. 75 GHz 10. 70 - 12. 75 GHz 10. 95 – 12. 75 GHz Frequency Transmitting 13. 75 - 14. 50 GHz 13. 75 - 14. 5 GHz 13. 75 – 14. 5 GHz Pedestal 360 Degree Azimuth Mount Tracking Performance 2 Axis Az/El FCC VMES Compliant (< 0. 20° - 99% of the time during Churchville B conditions EI angle < 80°) NA ≤ 0. 1° RMS Size 27. 5" x 37. 5" 37. 5 x 27. 5 x 14. 5 inches 49" x 51" Supply Voltage 28 V NA Power 336 W cont, 1260 W peak 3000 W peak NA Weight 182 lbs 60 -85 lbs depending on options 300 lbs MSD I - Team P 15310 - Satcom on the Move 12

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* Customer Requirement Number Importance CR 01 9 Demonstration of Geo-PNT System Accuracy CR 02 9 Demonstration of Geo-PNT Accuracy Loss over time during a “fade” CR 03 3 Video Report/Commercial (Visual Test Report) CR 04 1 Vehicle to provide movement of Geo-PNT CR 05 9 Demonstrate Full Range of motion of Geo-PNT CR 06 9 Closed Loop Control, based on Geo-PNT input CR 07 1 Complete documentation of how to operate the entire system CR 08 9 Complete documentation of system performance MSD I - Team P 15310 - Satcom on the Move Description 14

* Engineering Requirement Number Importance ER 1. 1 9 ER 1. 2 ER 1. 3 Engineering Requirement Unit of Measure Marginal Value Accuracy and minimum angular error of attitudes roll and pitch Degrees 2. 5 9 9 Accuracy of attitude yaw Position accuracy error horizontal Degrees Meters 2. 5 1. 5 ER 1. 4 9 Position accuracy error vertical Meters 2. 5 ER 1. 5 9 Position accuracy error velocity Meters/second 1. 5 ER 2. 1 9 Degrees/hour 3 ER 2. 2 9 Accuracy of error over time of attitudes roll and pitch Accuracy of error over time of attitude yaw Degrees/hour 3 ER 3. 1 ER 4. 1 3 1 Number of videos per demo Geo-PNT is mounted to a mobile object Number Meters/second 1 >0 ER 5. 1 ER 5. 2 ER 6. 1 9 9 9 Motion in yaw Motion in pitch and roll System functionality continues without user intervention Degrees N/A 360 180 Indefinite ER 7. 1 ER 8. 1 3 3 Provide a user manual Provide a written and visual test report N/A Y/N MSD I - Team P 15310 - Satcom on the Move 15

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*Benchmarking Frequecy Recieving Frequency Transmitting General Dynamics X Band SATCOM on the Move 10. 95 - 12. 75 GHz 13. 75 - 14. 50 GHz Pedestal 2 Axis Az/El Tracking Performance Size Supply Voltage Power Weight DRS Technologies SATCOM on the move (2 Port Cross Pol Ku- Rockwell Collins SWE-DISH Band) SATCOM On-The-Move CCT Coblam EXPLORER 9092 M 10. 70 - 12. 75 GHz 10. 95 – 12. 75 GHz 10. 95 -12. 75 GHz 13. 75 - 14. 5 GHz 13. 75 – 14. 5 GHz 13. 75 -14. 5 360 Degree Azimuth Mount FCC VMES Compliant (< 0. 20° - 99% of the time during Churchville B conditions EI angle < 80°) NA 27. 5" x 37. 5" 37. 5 x 27. 5 x 14. 5 inches 28 V DC 336 W cont, 1260 W peak 3000 W peak 182 lbs 60 -85 lbs depending on options MSD I - Team P 15310 - Satcom on the Move ≤ 0. 1° RMS 49" x 51" NA NA 308 lbs Acceleration • >200°/s Velocity • >100°/s (19” x 8” x 1. 8”) 90 / 264 V AC 1000 W 8. 5 lbs.

* Criteria Effectiveness Ease of Implementation Availability Power Efficiency Reliability Cost Effective Description Is the sub-component going to be effective at it’s intended function? Will the sub-component be easy to integrate into the system as a whole? Is the sub-component frequently used in other applications? Will the sub-component draw a lot of power? Does the sub-component have a known history of malfunctioning? Does the sub-component fit into the given budget for the project? Safe/Easy to Operate Is the sub-component pose any potential hazardous or harmful situations in any way? Is this easy to use? Weight Does the sub-component weigh too much for this application? Size Efficiency Is the sub-component’s size too large for the potential application? MSD I - Team P 15310 - Satcom on the Move 22

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* * Invoke Motion * Support the System *Power the Device * Support the Pointer * Receive Geo-PNT Data * Process Geo-PNT Signal * Direct Device * Point Device MSD I - Team P 15310 - Satcom on the Move 24

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* Mechanism Description Car Alternate: RC Car MSD I - Team P 15310 - Satcom on the Move • Car offers us a portable, readily accessible solution • Can go long distances at fast and slow speeds • Can handle larger weight tolerances • Offers similar solution to car, but cannot go as long of distance • Cannot go as far/fast • Harder to control 26

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* Mechanism Description Metal Box (Enclosure) • • Alternate: Wooden Box • Insulated • Not as easy to work with MSD I - Team P 15310 - Satcom on the Move Fit entire system into metal box Sturdy Portable Relatively cheap 28

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* Mechanism Description Battery Alternate: Power Supply MSD I - Team P 15310 - Satcom on the Move • • Most portable solution Easy to apply to system Cost effective Right choice in battery can power Geo. PNT, microcontroller, and motorized mount • Offers the same feasibility of implementation and advantages as the battery • Not portable, as 120 Vac connection required • Cost effective and more available than a battery 30

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* Mechanism Description Azimuth Mount • Large size for Telescope • Full range of motion • Very expensive • Easy to integrate Alternate: Azimuth Mount for Security Cam MSD I - Team P 15310 - Satcom on the Move • • Small size Full range of motion Light weight Easy to integrate 32

* Mechanism Alternate: 3 Axis Video Camera Mount MSD I - Team P 15310 - Satcom on the Move Description • • Large size Full range of motion Maintains camera frame to horizon Expensive 33

* Feasibility Analysis Support the Pointer MSD I - Team P 15310 - Satcom on the Move

* Feasibility Analysis Support the Pointer MSD I - Team P 15310 - Satcom on the Move

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* Mechanism Description Ethernet Alternate: Serial Cable MSD I - Team P 15310 - Satcom on the Move • One Ethernet cable interface • Standard port on microcontroller dev boards and laptops • Can handle Geo-PNT’s maximum data output easily • Three serial cable interface • Dev boards with multiple ports are larger and rarer • Not standard on Laptops • Can handle Geo-PNT’s maximum data output easily 37

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* Mechanism Description Microcontroller • • • Alternate: Laptop MSD I - Team P 15310 - Satcom on the Move Portable and easy to use option. Does not need significant power Inexpensive Handles data processing needs Will interface with Geo-PNT Good for real-world testing and development • Easy to use and readily available • Development work with microcontroller will interface with laptop • Does all the microcontroller can do at the cost of mobility • Added benefit – ease of displaying data during development phase 39

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* Mechanism Description Camera Alternate: Laser Pointer MSD I - Team P 15310 - Satcom on the Move • Visually appealing • Data can be directly placed into the video • Small, sturdy, made for movement • Easy to mount • Internal battery source • Harder to tell where it’s pointing • • • Visually appealing Shows line of sight Easy to mount Internal battery source Easy to tell where it’s pointing 42

*Option One Advantages: * Extra Axis - Camera orientation control * Video of pointing data * Smaller overall system Disadvantages * More difficult to monitor system * Extra Axis - Harder to program MSD I - Team P 15310 - Satcom on the Move

*Option Two Advantages: * Obvious line of site * 2 Axis - Simpler to control * Easier to monitor system Disadvantages * Laser is less presentable * 2 Axis - Camera video will not have a horizontal horizon line * Less mobile MSD I - Team P 15310 - Satcom on the Move

* Engineering Requirement Unit of Measure Marginal Value Accuracy and Minimum Angular Error of Attitudes Roll and Pitch degrees 2. 5 Accuracy of Attitude Yaw degrees 2. 5 Position Accuracy Error Horizontal meters 1. 5 Position Accuracy Error Vertical meters 2. 5 Position Accuracy Error Velocity meters/sec 0. 1 Test (how are you going to verify satisfaction) Visual Measurement based on Aiming device ability to point at specified target Visual Measurement based on Aiming device ability to point at specified target Accuracy of Error Over Time of Attitudes Roll and Pitch degrees/hr 3 Accuracy of Error Over Time of Attitude Yaw Number of Videos per Demo Geo-PNT is Mounted to a Mobile Object degrees/hr number meters/sec 3 1 >0 Motion in Yaw degrees 360 Motion in Pitch and Roll degrees 180 Time-trial Visual Measurement based on Aiming device ability to point at specified target Time-trial of Visual Measurement based on Aiming device ability to point at specified target N/A Basic Observation Range of Motion Measurement and Analysis indefinate Y/N N/A N/A System Continues without MSDFunctionality I - Team P 15310 - Satcom on. User the Intervention Move Provide User Manual Provide Written and Visual Test Reports 45 N/A N/A

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