Inertial Navigation Enhanced - Honeywell · PDF fileE-SIGI Enhanced Space Integrated GPS/INS Inertial Navigation System with Embedded GPS Receiver and Mission Computer Integrated global

E-SIGI Enhanced

SpaceIntegrated GPS/INS

Inertial NavigationSystem withEmbedded GPSReceiver and Mission Computer

Integrated global positioning/inertial navigationsystem (GPS/INS) and Mission Computer thatmeet rigid criteria for reliability, performance, spaceradiation tolerance and cost

Mission Computer features PowerPC 603e and VxWorksfor hosting application software such as guidanceand control

12-channel all-in-view GPS receiver withSPS/PPS capabilityHighly accurate navigation-grade inertial sensors

Triple navigation solutions: pure inertial, GPS-only,and blended GPS/INS

Differential GPS option for precision landing

Expansion slot accommodates application-specificinputs/outputs

Navigation system qualified to launch vehicle,on-orbit and re-entry vehicle environments

Based on existing high-volume militaryproduction line

Flexible hardware and software system architectureadaptable to varied missions including: • Reusable Launch Vehicles • Expendable Launch Vehicles • Space Transportation Vehicles • Rendezvous and Docking • Re-Entry Vehicles • Target Vehicles • Range Tracking

Aerospace Electronic Systemsense Def & Space Electronic Systems

Honeywell13350 U. S. Highway 19 NorthClearwater, FL 33764-7290Tel: 727-539-4000http://www.honeywell.com/space

June 2004 DFOISR: 04-S-1703

Printed in U.S.A. on Recycled Paper

© 2004 Honeywell Inc

System Characteristics

Enhanced Space Integrated GPS/INS – E-SIGI

* Mission specific -PowerPC is a registered trademark of Motorola. VxWorks is a registered trademark ofWind River Systems, Inc.

Form Factor....................................7 x 7 x 9.8 inchesWeight..............................................................< 21 lbsPower Requirements* +28 Vdc operation.................................34 to 45 wattsThermal Operating Range* Ambient air......................................... .-54ºC to +71ºC (+95ºC 30 minutes) Space vacuum, cold plate interface.....-54ºC to +55ºCMTBF*.......................................................20,000 hours

Navigation Performance Mission Computer Performance

Processor Motorola MPC 8240 >100 MIPSMemory 32MB SDRAM memory (4Mx64) 8MB Flash memory (2Mx32) 128K x 8 EEPROM history memoryOperating System VxWorks Tornado Development EnvironmentInterfaces.............MC 1553B (BC or RT) 7 RS422 Serial Data Bus 8 discrete inputs 8 discrete outputs

Overall Performance...............better than 0.01 deg/hrGPS and GPS/INS Blended Performance (SA off)* Position accuracy....................(SEP) better than 50 m Velocity accuracy (RMS)............better than 0.3 m/secAlignment Time* Gyrocompass...............................................4 minutesOperating Ranges Altitude............................................600 nautical miles Angular Rate..........................................±360 deg/sec >±600 deg/sec*Linear Velocity................................±12000 meters/secAngular Acceleration..............................±171 deg/sec2

Linear Acceleration................................................±10g >±100g*Jerk....................................................±100 meters/sec3

Interfaces..................................Nav 1553B (RT or BC) RS422 Serial Data Bus

MCProcessor

NavProcessor

Nav 1553

MC 1553

High SpeedSerial (7)Discrete

(8 In/8 Out)Custom I/O

DPRAMSerialPort

Serial Port RF

28 Vdc InertialElectronics

SIGIIMU

Force 5GPS

PPS or SPS

PowerSupply

CustomBoard

DPRAMGPS Module

IE Assembly

ISAIMM Processor

Custom Board

MCDC PowerSupply

Chassis

Battery Cover