GPS Wing approval must be granted prior to operational use or export.Cleared by DoD/OSR for public release under OSR Case No. 07-S-1631 on June 11, 2007.

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I S R > G O V E R N M E N T S E R V I C E S > A M & M > S P E C I A L I Z E D P R O D U C T S

I n t e r s t a t e E l e c t r o n i c s

T R U T R A K ™ E V O L U T I O N

F E A T U R E S A N D B E N E F I T S

• Provides cost, size, power reduction, and M-Code

transition opportunity to user community

• Designed to support highly integrated guidanc e

solutions

• Direct Deep Integration supports direct acquisition

and tracking in a high A/J environment

• Contains Core GPS Capabilities plus On-chip User

Application Processor

Core Summary

• 24 -channel L1 /L2 GPS SAASM receive r

• Processes Coarse Acquisition (C/A) and encrypted

P(Y) code signals

• Tracks all satellites in view

• ULTRA FAST Direct Y-code acquisition when keyed

and initialize d

• Direct path to M-Code

• Temperature sensors on chip

• 20,000 G gun shock survivability

• Implements SS-GPS-001SAASM security

requirements

• Programmable power control options

• Requires only external antenna and power

User Application Processor Summary

• On-chip capacity for guidance, canard control, etc.

• Power PC 440 with DPFP and DSP instructions

• 2 MBytes program/data memory with SAASM

memory separation

• I/O Ports :

– 4 Serial RS-422 Ports, GPS and PC baud rates

supported

– External Memory Address Bus

– Up to 800 MByte/sec interface to GPS engine

– Serial IMU port (SDLC or AMRAAM)

– 16 programmable I/O

Discretes

• CPU rate: 25, 50 , 100,

200 MHz

Programmable

• Cache: 32K bytes

instruction/32KBytes

data

• TraceBus and JTAG

development interfaces