amcom mk66 guidance module 04-12-2005. software block diagram data handler imu processinggps...

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AMCOM MK66 AMCOM MK66 Guidance Module Guidance Module 04-12-2005 04-12-2005

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AMCOM MK66 AMCOM MK66 Guidance ModuleGuidance Module

04-12-200504-12-2005

Software Block DiagramSoftware Block Diagram

Data Handler

IMU Processing GPS Processing RMS Control

Serial I/O Ctrl

Parallel Ctrl.Actuate, Deploy

Course Plot/Corr.

RS-232 Dev

SimulationSimulationPhase 1Phase 1

RS232

FPGA “simulator”(program runs here)

Navionic input simulation

SimulationSimulationPhase 2Phase 2

RS232

FPGA runs flight software Navionic input simulation

Servomotor ControlServomotor Control

Altera knows NOTHING of servomotor Altera knows NOTHING of servomotor positionposition

FPGA sends control line to FPGA sends control line to servomotor, continues to hold line servomotor, continues to hold line level.level.

Servomotor stops at designated Servomotor stops at designated position while line level is high.position while line level is high.

ServoblockServoblock

Servo

Parallel Port

Ctrl. Logic

Power Conv.

Feedback

Complete Avionics ModuleComplete Avionics Module Avionics Module

ADDITION TO HYDRA 70 ROCKET

Male and Female Male and Female InterfacesInterfaces

-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)

Canard AssemblyCanard AssemblyCanard Assembly

Canard Assembly Cont…Canard Assembly Cont…

Canard and actuation mechanism shown

- actuation gear attaches to assembly here

CANARD

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

ACTUATION MECHANISM COMPONENTS

Springs for deployment and locking mechanism to prevent canard from closing once deployed

Yellow piece here is attachment point to frame

CANARD IN CLOSED POSITION

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

CANARD MOUNTING LOCATION

Mounting bar offset 45 deg from frame to accommodate canard assembly and servomotors

Placement of Canard Assembly

Placement of Servomotors

-Mounts for servomotors currently being designed

-Servos mounted at angle to line up proper angle with actuation gear

Packaging inside module shell

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

GPS and CPU attach on either side of frame

AVIONICS MODULE INTERNAL VIEWAVIONICS MODULE INTERNAL VIEW