Criteria

Performance Criteria: Adopted from Mission Concept Review (MCR)

  • The AEV will begin at the starting dock and move forward 14 ft to stop at the gate where it will pause for 7 seconds
  • The AEV will then travel forward another 14 ft to the loading zone where it will  magnetically attach to the load and pause for 5 seconds
  • The AEV will then return to the gate pausing again for 7 seconds
  • The AEV will then return to the starting dock and will stop there

AEV Course Map

Performance Considerations:

  • 6 feet from the starting dock, the AEV will encounter a 2.39 degree incline for 4 feet
  • 4 feet from the gate, the AEV will encounter a 1.19 degree decline for 4 feet
  • On the way back, connected to the load, the AEV will have to traverse these slopes; therefore, a flexible connecting point should be considered to ensure the load doesn’t break free from the AEV
  • Coming down from the decline into the loading zone, there needs to be minimal recoil when the AEV attaches to the load, therefore, breaks/reversing of the propellers should be considered to slow down the AEV

AEV Course Specifications (MCR, p4)

Additional Criteria: Adopted from Mission Concept Review (MCR)

  • The AEV must complete the circuit (get the load and return) within 2.5 minutes
  • The magnet that will attach to the load must be at least 2 inches from the Arduino

The other large criteria deals with the money involved and further time constraints, found in the budget.