1 / 11

Team 01 : QuadSquad Safety and Reliability

Team 01 : QuadSquad Safety and Reliability. Andrew Boldt. Abstract. Android controlled quadcopter Bluetooth connection (~300 foot range) GPS , compass , ultrasonic , battery monitor Brushless DC motors with speed controllers PWM input flight controller board for stabilization

willis
Download Presentation

Team 01 : QuadSquad Safety and Reliability

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript

  1. Team 01 : QuadSquadSafety and Reliability Andrew Boldt the ECE quadcopter senior design project @ Purdue University

  2. Abstract • Android controlled quadcopter • Bluetooth connection (~300 foot range) • GPS, compass, ultrasonic, battery monitor • Brushless DC motors with speed controllers • PWM input flight controller board for stabilization • Waypoint navigation & auto take-off/land the ECE quadcopter senior design project @ Purdue University

  3. the ECE quadcopter senior design project @ Purdue University

  4. Project-Specific Success Criteria An ability to … • determine the position of the quadcopter using GPS • control the copter using an Android device over a Bluetooth interface • automatically take-off and land • fly-by-waypoint using GPS coordinates • monitor the state of battery charge and relay back to user the ECE quadcopter senior design project @ Purdue University

  5. Criticality Levels • Total Quadcopter Meltdown • Battery/ESC/Flight Controller short • Severe impact to flight • Crash into person • λ < 10^-9 • Criticality Level I • Basic Component Failure • Micro/GPS/MAG/ULTRA failure • Quadcopter hovers • λ< 10^-6 • Criticality Level IV the ECE quadcopter senior design project @ Purdue University

  6. Components Monitored • Microcontroller • Power SupplyChip • Line Level Chip • ESC’s the ECE quadcopter senior design project @ Purdue University

  7. FMECA - Micro the ECE quadcopter senior design project @ Purdue University

  8. FMECA - Power the ECE quadcopter senior design project @ Purdue University

  9. FMECA - Line the ECE quadcopter senior design project @ Purdue University

  10. FMECA – ESC’s the ECE quadcopter senior design project @ Purdue University

  11. Questions?? the ECE quadcopter senior design project @ Purdue University

More Related