LASEREF VI Micro Inertial Reference Systems
Overview
LASEREF VI inertial reference unit (IRU) offers on-aircraft data load capability, HIGH Step II software for 100% availability of low required navigation performance authorized required (RNP AR) with integrity coasting, automatic dependent surveillance-broadcast (ADS-B) compliance with civil certified global navigation satellite system (GNSS) receiver & automatic mode control with align-in-motion.
Our LASEREF VI is the smallest, lightest and lowest power IRU on the market. It is one-half-the-size, one-third-the-weight and requires one-third-the-power than the LASEREF IV. The system is available for rotorcraft and fixed-wing applications.
Other key elements include:
Our LASEREF VI is the smallest, lightest and lowest power IRU on the market. It is one-half-the-size, one-third-the-weight and requires one-third-the-power than the LASEREF IV. The system is available for rotorcraft and fixed-wing applications.
Other key elements include:
- Automatic mode control logic and initialization
- Optimal sensor performance to provide the best performance for high bandwidth SATCOM (e.g. JETWAVE SATCOM), SVS (Synthetic Vision System), CVS (Combined Vision System), and HUD (Heads Up Display)
- Meets both fixed wing and rotary wing environmental and electromagnetic environments
- Passively cooled - avoiding cost and space for cooling fans
- On-aircraft data load capability
- Honeywell's inertial GPS hybrid (HIGH) integrity coasting provides 100% availability of RNP AR navigation and can eliminate predictive receiver autonomous integrity monitoring (RAIM) for non-precision GPS approaches
- Installation configurable features such as lever arm compensations and selectable output filtering eases integration and installation into existing aircraft
Compatible Aircraft
Airbus Helicopter H145
Airbus Helicopter H225
Boeing 777X
Boeing 787
Bombardier C-Series
Bombardier CRJ-100/200/700/900
Bombardier Challenger 350
Bombardier Challenger 605
Bombardier Global 6000
Bombardier Global 7000
Bombardier Global 8000
Bombardier Q400
COMAC ARJ-21
COMAC C919
Cessna Latitude
Cessna Longitude
Civilian C-130
Dassault Falcon 2000EX
Dassault Falcon 900EX
Dassault Falcon F5X
Dassault Falcon F8X
Embraer 170/175/190/195
Embraer E2
Gulfstream G280
Gulfstream G350
Gulfstream G450
Gulfstream G500
Gulfstream G550
Gulfstream G650
Hawker-Beachcraft Hawker 4000
Hawker-Beachcraft Hawker T-6B
Irkut MC-21
Leonardo AW-101
Leonardo M-345
Mitsubishi Regional Jet
Pilatus PC-21
Pilatus PC-7
Pilatus PC-9 Trainer
Sukhoi Superjet 100
Specifications
Key Differentiators
- Certifications
- Hardware Certification - DO160G
- Software Certification - DO178B Level A
- Features & Benefits
- Now provides 100% Availability of RNP 0.1 NM Navigation
- Provides recovery of full performance mode following loss of power in flight
- Smallest, lightest, and lowest power IRS in the industry
Dimensions
- Weight
- 9.3 lbs
- Dimensions
- 6.5”W x 6.4”L x 6.4”H
- Size
- 267 cubic inches millimetre
Performance Data
- Power
- 20 watts Watt
- Mounting tray
- Electronic mounting tray alignment
- Mean Time Between Failures (MTBF)
- 25,000 operational hours
- Interface
- 4 ARINC 429 Transmitters (Can support up to 80 different LRUs)
- 7 ARINC 429 Receivers
- Ethernet Ports
- 1
- Discrete Outputs
- 2
- Discrete Inputs
- 12
- Cooling
- Passive
- Components
- HG2100BB Micro IRU
- IM-950 Aircraft Personality Module
- WG2001 Mounting Tray
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