1. AMCOM MK66 Guidance Module

2. IMU Converting acceleration information to position data
Performing double integration
Using rectangular integration method
Ready for testing and integration into simulation software

3. Software optimization
Subroutine optimization
Computational requirement reduction
In-memory space reduction
Completion of roll compensation

4. Software: What’s left Completion of serial I/O routines
Integration of IMU code module
Serial-based testing

5. Canard/Canard Cam Design
One-piece construction
Built-in mechanical stop
NACA airfoil to be CNCed
Fillet right angles to reduce stress concentrations

6. Canard Actuation Mechanism
Machined as four basic components
Positive stop built into upper box half
Locks canard at 90 degrees
Size: .75” x .4”

11. Frame Machined from single piece of material (13/16” thick)
Canard Mechanism mount oriented at 45 degree angle
.707” thick at maximum
.25” thick frame bulk
Symmetrical
Fillets to reduce stress concentrations

12. Avionics Module

13. Avionics Module

14. Avionics Module

15. Gear Selection Miter gear pair (non-backdriving)
1” pitch diameter on larger gear (mounted to canard mechanism)
.5” pitch diameter on smaller gear (mounted to servomotor)

16. To Do Finish designing gear mount
Order helical torsion spring, frame material, canard actuation material
Meet with AMCOM
Machine