AMCOM MK66 Guidance Module

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Presentation transcript:

AMCOM MK66 Guidance Module 04-05-2005

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

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

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

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

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

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

Avionics Module

Avionics Module

Avionics Module

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)

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