- For performance test one, Team K was focusing on choosing the final AEV design. First, two design prototypes were chosen according to the creative design process from the Preliminary R&D.
- The first prototype has vertical wings and a T-shape base as seen below.
Figure 1: Design A
- The second prototype has diagonal wings and a T-shape base seen below.
Figure 2: Design B
- A uniform set of code was used for testing those two prototypes:
- The plots of Power vs. Time and Power vs. Distance of those two design are provided below.
Figure 3: power vs. time for performance test 1
Figure 4: power vs. distance for performance test 1
Blue line: Design A
Red line: Design B
- By using the MATLAB analysis tool, the energy used by Design A was found to be 64.194 joules, and the energy used by Design B was 72.196 joules.
- The figures Power vs. Time and Power vs. Distance also show that Design A used less power than Design B, especially for the coasting part, which is between 19 seconds and 24 seconds. Overall, the power used by Design A was much less than the power used by Design B.
- The concept scoring for Designs A and B is presented below.
- By observation of each team member, Design B started slower than Design A during acceleration.
- The stability and safety of Design A and Design B were almost the same.
- In conclusion, Design A has been chosen for future testing.