LASEREF VI Micro Inertial Reference System Special Missions
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
Benefits
- Automatic mode control logic and initialization
- 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
- Meets both fixed wing and rotary wing environmental and electromagnetic environments
- On-aircraft data load capability
- Optimal sensor performance to provide the best performance for high bandwidth SATCOM (eg JETWAVE SATCOM), SVS (Synthetic Vision System), CVS (Combined Vision System), and HUD (Heads Up Display)
- Passively cooled - avoiding cost and space for cooling fans
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
Size
- 6.52 in x 6.43 in x 6.28 in
Mounting
- 0.5 lbs
Heading
- 0.1 degree 2o- output at 50Hz
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