Navigation Systems
LASEREF VI Micro Inertial Reference System Special Missions
LASEREF VI Micro Inertial Reference System Special Missions
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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:
• 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
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
Specifications
Power and Electrical
- Power
- 20 watts
Performance
- Hybrid position coasting performance
- >20 minutes @ RNP 0.3 NM
- Accelerometer Sensor Technology
- Quartz
- Gyro sensor technology
- GG 1320 digital ring laser
- Position (inertial)
- 0.8 NMPH CEP or 1.67 NMPH R95 (nautical miles per hour)
- Position (hybrid)
- Typically <18 Meters 2DRMS
- Key Benefits
- Automatic mode control logic and automatic initialization for reduced crew workload and elimination of mode select unit
- Enhanced automatic realignment uses GPS to refine alignment between flights.
- Integrated vertical acceleration output for integration with flight inspection equipment
- Provides protection from GNSS-denied environments
- Industry
- Commercial
- Cooling
- Passive
Connectivity and Systems
- Velocity (inertial)
- 6 knots R95
- Velocity (hybrid)
- 0.25 knots R95
- Components
- HG2195BB Micro IRU
- IM-950 Aircraft Personality Module
- WG2001 Mounting Tray
- Interface
- ARINC 429 configurable inputs, high speed outputs
- Designed for integration into flight inspection equipment
Certification
- Certifications
- Environmental/EMC qualification: DO-160G, now including typical helicopter environments (i.e., vibration for helicopters with unknown rotor frequencies, salt spray, sand and dust etc.)
- Hardware certification: DO-254 Level A
- Software certification: DO-178B Level A
- Technical standard order (TSO and ETSO): C3e, C4c, C5f, C6e, C196b
Physical
- Mounting tray
- 0.5 lbs
- Dimensions
- 6.52 in x 6.43 in x 6.28 in
- Heading
- 0.1 degree 2o- output at 50Hz
- Weight
- < 9.0 lbs (4.1 kg)
- Volume
- <265 cubic in (4.32 liters)
- <265 cubic inches (4.32 liters)
Mechanical
- Attitude
- 0.05 degree 2o- (two sigma 95% accuracy) output at 100Hz
Power and Electrical
- Power
- 20 watts
Performance
- Hybrid position coasting performance
- >20 minutes @ RNP 0.3 NM
- Accelerometer Sensor Technology
- Quartz
- Gyro sensor technology
- GG 1320 digital ring laser
- Position (inertial)
- 0.8 NMPH CEP or 1.67 NMPH R95 (nautical miles per hour)
- Position (hybrid)
- Typically <18 Meters 2DRMS
- Key Benefits
- Automatic mode control logic and automatic initialization for reduced crew workload and elimination of mode select unit
- Enhanced automatic realignment uses GPS to refine alignment between flights.
- Integrated vertical acceleration output for integration with flight inspection equipment
- Provides protection from GNSS-denied environments
- Industry
- Commercial
- Cooling
- Passive
Connectivity and Systems
- Velocity (inertial)
- 6 knots R95
- Velocity (hybrid)
- 0.25 knots R95
- Components
- HG2195BB Micro IRU
- IM-950 Aircraft Personality Module
- WG2001 Mounting Tray
- Interface
- ARINC 429 configurable inputs, high speed outputs
- Designed for integration into flight inspection equipment
Certification
- Certifications
- Environmental/EMC qualification: DO-160G, now including typical helicopter environments (i.e., vibration for helicopters with unknown rotor frequencies, salt spray, sand and dust etc.)
- Hardware certification: DO-254 Level A
- Software certification: DO-178B Level A
- Technical standard order (TSO and ETSO): C3e, C4c, C5f, C6e, C196b
Physical
- Mounting tray
- 0.5 lbs
- Dimensions
- 6.52 in x 6.43 in x 6.28 in
- Heading
- 0.1 degree 2o- output at 50Hz
- Weight
- < 9.0 lbs (4.1 kg)
- Volume
- <265 cubic in (4.32 liters)
- <265 cubic inches (4.32 liters)
Mechanical
- Attitude
- 0.05 degree 2o- (two sigma 95% accuracy) output at 100Hz
- Power : 20 watts
- Hybrid position coasting performance : >20 minutes @ RNP 0.3 NM
- Accelerometer Sensor Technology : Quartz
- Gyro sensor technology : GG 1320 digital ring laser
- Velocity (inertial) : 6 knots R95
- Position (inertial) : 0.8 NMPH CEP or 1.67 NMPH R95 (nautical miles per hour)
- Velocity (hybrid) : 0.25 knots R95
- Position (hybrid) : Typically <18 Meters 2DRMS
- Certifications : Environmental/EMC qualification: DO-160G, now including typical helicopter environments (i.e., vibration for helicopters with unknown rotor frequencies, salt spray, sand and dust etc.)|Hardware certification: DO-254 Level A|Software certification: DO-178B Level A|Technical standard order (TSO and ETSO): C3e, C4c, C5f, C6e, C196b
- Mounting tray : 0.5 lbs
- Key Benefits : Automatic mode control logic and automatic initialization for reduced crew workload and elimination of mode select unit|Enhanced automatic realignment uses GPS to refine alignment between flights.|Integrated vertical acceleration output for integration with flight inspection equipment|Provides protection from GNSS-denied environments
- Dimensions : 6.52 in x 6.43 in x 6.28 in
- Components : HG2195BB Micro IRU|IM-950 Aircraft Personality Module|WG2001 Mounting Tray
- Interface : ARINC 429 configurable inputs, high speed outputs|Designed for integration into flight inspection equipment
- Industry : Commercial
- Attitude : 0.05 degree 2o- (two sigma 95% accuracy) output at 100Hz
- Heading : 0.1 degree 2o- output at 50Hz
- Cooling : Passive
- Weight : < 9.0 lbs (4.1 kg)
- Volume : <265 cubic in (4.32 liters)|<265 cubic inches (4.32 liters)
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