1. AMCOM MK66 Guidance Module 04-12-2005

2. Software Block Diagram Data Handler IMU ProcessingGPS ProcessingRMS Control Serial I/O Ctrl Parallel Ctrl.Actuate, Deploy Course Plot/Corr. RS-232 Dev

3. Simulation Phase 1 RS232 FPGA “simulator” (program runs here) Navionic input simulation

4. Simulation Phase 2 RS232 FPGA runs flight software Navionic input simulation

5. Servomotor Control Altera knows NOTHING of servomotor position Altera knows NOTHING of servomotor position FPGA sends control line to servomotor, continues to hold line level. FPGA sends control line to servomotor, continues to hold line level. Servomotor stops at designated position while line level is high. Servomotor stops at designated position while line level is high.

6. Servoblock Servo Parallel Port Ctrl. Logic Power Conv. Feedback

7. Complete Avionics Module Avionics Module ADDITION TO HYDRA 70 ROCKET

8. Male and Female Interfaces -Acme Stub Threads with a pitch of 6 -Half inch interference zones for placement in warhead/motor -All dimensions made to match current rocket interfaces precisely -Threaded push pins used to secure interfaces to module shell (not shown)

9. Canard Assembly

10. Canard Assembly Cont… Canard and actuation mechanism shown - actuation gear attaches to assembly here

11. CANARD Machined from a single piece of material for simplicity and added strength

12. ACTUATION MECHANISM COMPONENTS Springs for deployment and locking mechanism to prevent canard from closing once deployed

16. Yellow piece here is attachment point to frame

17. CANARD IN CLOSED POSITION

18. Internal Frame -Machined from solid piece of aluminum -Allows for placement of IMU, GPS, and CPU -Machined from solid piece of aluminum -Allows for placement of IMU, GPS, and CPU Internal Frame

19. CANARD MOUNTING LOCATION Mounting bar offset 45 deg from frame to accommodate canard assembly and servomotors

20. Placement of Canard Assembly

21. Placement of Servomotors -Mounts for servomotors currently being designed -Servos mounted at angle to line up proper angle with actuation gear

22. Packaging inside module shell

23. FRAME WITH ELECTRONICS -Thermal battery and insulation (red) attach to end of frame -IMU attaches inside of frame -Thermal battery and insulation (red) attach to end of frame -IMU attaches inside of frame FRAME WITH ELECTRONICS

24. GPS and CPU attach on either side of frame

25. AVIONICS MODULE INTERNAL VIEW