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Power Available vs. Required for Standalone Low Cost Flight Display - PowerPoint PPT Presentation

Power Available vs. Required for Standalone Low Cost Flight Display System Who are We? EE Team #192 ME Team #34 Gao Cai Justin Dubrosky Dylan Hammerman Brandon Naples Andrew Radlbeck Faculty Advisor : Chengyu Cao Shu Wan Faculty


  1. Power Available vs. Required for Standalone Low Cost Flight Display System

  2. Who are We? EE Team #192 ME Team #34 Gao Cai Justin Dubrosky Dylan Hammerman Brandon Naples Andrew Radlbeck Faculty Advisor : Chengyu Cao Shu Wan Faculty Advisor: Helena Silva Sikorsky Liaison Paul Inguanti

  3. Introduction Design a stand alone unit to determine the ceiling IGE at specific weights for low cost helicopters. Requirements: ● Continuous atmospheric pressure and air temperature measurements ● Altitude calculation ● Ceiling IGE ● Indicator: LED and LCD ● Accurate and repeatable function ● Low cost and lightweight ● Portable (self-powered)

  4. Helicopter Pictures Schweizer S-300C

  5. Design: Old Prototype I 2 C ● Data Logging Unit SPI ● Records altitude/temperature data onto an SD card Elevator Altitude ● Data easily graphable in Excel ● This graph represents the ≈ 18m altitude of the back ITEB elevator shaft from “C” to “4”

  6. Design: Old Concept GPIO I 2 C SPI

  7. Design: Final I 2 C SPI GPIO SPI

  8. Code Snippets ● Main control unit code

  9. Code Snippets ● Sensor control unit

  10. Schematics

  11. Schematics (cont)

  12. Schematics (cont) TI PCA9544

  13. Schematics (cont)

  14. Design: Mechanical Specs ● 6061 Aluminum ○ light and low cost [A] ● Dimensions ○ 6” diameter & 2.5” height Construction A. Top Plate: Cut-outs for the pressure sensors B. Center: To create enclosure for all [B] electrical components C. Base Plate: Board is mounted here [C]

  15. Simulations: Mechanical

  16. Results

  17. Results

  18. Results

  19. Results

  20. The Future ● Interfacing -- Control & Sensor ● Velocity Testing ● Altitude testing ○ Low - offset calculation ○ High - final test

  21. Schedule Begin Winter Finish Winter Presentation 2 Order Parts Assemble Code for Winter Break Testing 1/21 Testing 1/25 12/3 12/4 SAM D20 12/5 12/15-1/21 Design Begin Spring Finish Spring Report and Poster Project Complete Modification Spring Break Testing 02/14 Testing 03/28 04/01 05/02 02/01 03/16 - 22 *Not to Scale

  22. Budget ● Sikorsky → $4,000 budget ● Prototyping cost breakdown: - Adapter Board $5 - Battery $24 - Breadboard/wires $20 - Charger $8 - Development/Debugger board $30 - Enclosure $90 - Keypad $4 - LCD $25 - Multiplexer Free - Sensors $90 - SD Card $13 Total: $309

  23. Cost per Unit - Enclosure $90 - Four Sensors $60 - LCD $25 - Two batteries $24 - Microprocessors $20 - Charger $8 - Keypad $4 - Multiplexer $1 - Wires $1 Total: $233

  24. Questions?

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