Open UAS 1.0

A carbon fiber edtion of the OpenUAS project, built in 2020.

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More information can be found on the Laboratory for Temporal Logic Youtube Page (opens new window).

Requirements include:

1. Configurable: Wings can be changed
2. Can break down and moved easily
3. Simple assembly
4. Does not require a runway
5. Can be manufactured by hobbyist
6. Can withstand a crash landing

Design Goals

Development for design goals began in 2019.

Overall weight: 4.138 lbs

Lessons Learned

The next iteration must have the following capabilities:

• Better access to electronics
• Better flight characteristics
• Better reparability
• Tailwheel configuration is harder to control
• Better Manufacturability
• Better transportability (multiple piece wing)
• Better corrective action for left turning tendencies

Team

Team Members from left to right: Will Burken, John Edgren, Ellie Diersen, Marcella Anderson, Colton Glick, John Levandowski (not pictured), Christopher Johannsen (not pictured), Stephanie Jou (not pictured)

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