Project: Load testing base for testing engine output PART 1

Goal

Build a base that flight platforms can be attached to and have their maximum load bearing output tested in various ways in a controlled bench test environment. Ideally this could serve as a prototype for performing the same range of tests on other UAV platforms. This will be achieved by designing the base and attachment hardware, fabrication of brackets and mounting on an appropriate base.

Design Phase:

Primary Specifications:

• Quick attachment of drone legs to base.
• Sufficient weight to counter

Secondary Specifications:

- USB Power or at least potential for future.

Parts and Materials

• PLA Plastic
• Suitable surface (first blog post)
• USB pass through.

First Thoughts

This project began as a solution to the question of how to test the motors of a multirotor UAV with propellers attached, a very unsafe proposition at the best of time.  By creating a very secure but quick attachment of the UAV landing struts to a heavy base I can safely test multiple throttle output settings.  A USB to micro USB connection directly on the base provides a convienent connection for constant reboots, mavlink telemetry and firmware upgrades.  To begin I will photograph AG1's landing feet and take measurements, the summary of which will comprise the second blog post.