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Design / build / fly a fixed-wing RC aircraft from the ground up with a predefined payload and range.

A Kepler-level Aerospace Engineering project led by Raul Maldonado in collaboration with Aditya Ojha and Bryan Atanga.

Student Team: Vito "nufflee" Dz-P, Katherine Li, Aarush Das, Ishan Kumar, Gabriel Chapa and Aarish Rajwani

Sponsoring Patron: Nathan Bowyer

Began: June 9, 2020

Project Summary: The goal of this project is to design, build, and fly a Radio Controlled (RC) Aircraft from scratch. The aircraft will carry a payload to its destination. The design process will use a simplified simulation approach and the build process will use Commercial Off The Shelf (COTS) parts to ease the difficulty of aircraft design.

This project will lay a foundation of knowledge and techniques for possible future aerospace projects.

Project Repository: X1


An electric powered RC airplane will have the following requirements:

  • The aircraft shall be controlable and stable in flight
  • The aircraft shall be able to gather sensor data defined in the Sensor Package Capabilities
  • The aircraft shall satisfy the minumum performance metrics defined in the Aircraft Performance Metrics section
  • The aircraft shall be reasonably easy to transport and/or pack

Project Timeline

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"Short_Description": "Create CAD models of all of the selected sensor modules.", "Category": "task"},{"Title": "TSoG X1/Create an Aerodynamic Model", "Task_Status": "In Progress", "Priority": "Normal", "Task_Category": "TSoG X1/Sim", "Percent_Complete": 0, "Dependencies": "TSoG X1/Add Angle of Attack to State Vector", "Start_Date": "2020-07-08", "End_Date": "2020-07-13", "Task_Leader": "User:RaulM", "Members": "User:Nufflee", "Short_Description": "Convert our current static Aerodynamic forces into a dynamic model based on angle of attack", "Category": "task"},{"Title": "TSoG X1/Create an Atmosphere Model", "Task_Status": "Complete", "Priority": "Normal", "Task_Category": "TSoG X1/Sim", "Percent_Complete": 100, "Dependencies": "", "Start_Date": "2020-06-19", "End_Date": "2020-07-03", "Task_Leader": "", "Members": "User:Aarush26", "Short_Description": "Create an atmospheric model to calculate an estimate of the atmospheric conditions based on altitude.", "Category": "task"},{"Title": 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Detailed Performance Metrics

Aircraft Specifications

  • Cruising Altitude:
    • 25ft, MIN
    • 50ft, MID
    • 100ft, MAX
  • Payload Capacity:
    • Mass of Sensor Package (TBD), MIN
  • Flight Time:
    • 10 min, MIN
    • 30 min, MID
    • 60 min, MAX
  • Runway Takeoff Distance:
    • 250ft, MAX (the shorter the better)

Sensor Package Specifications

Sensor Package needs to be able to measure and record…

  • Angle of Attack (AoA), Sideslip
  • Airspeed (scalar)
  • Static Temperature of Air
  • Static Pressure of Air

Additional parameters that would be nice to measure and record include...

  • Dynamic Pressure of Air
  • Orientation of Aircraft
  • Position of Aircraft (ex. GPS)
  • Velocity of Aircraft (in vector form)

Project Posts

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