GNSS Interruption
Satellite loss in contested or obstructed environments.
Solutions / Aerospace Navigation
Integrated IMU, INS, FOG and sensor fusion systems for stable positioning, attitude control and mission continuity in demanding aerospace environments.
02
Key operating constraints that shape the solution architecture.
Satellite loss in contested or obstructed environments.
Stable output is required under harsh motion and temperature.
Compact, light and power-efficient systems are required.
03
A complete sensing, navigation and engineering stack.
IMU and FOG sensing inputs.
GNSS / INS and inertial navigation processing.
Drift suppression and state estimation.
Evaluation platform for integration and testing.
Validation, configuration and lifecycle support.
04
Mission-ready modules matched to this operating environment.
Fiber Optic Gyro Navigation System
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Tightly Coupled Navigation System
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GNSS / INS Navigation System
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Evaluation & Integration Platform
Request Kit ->05
Core technologies supporting reliable sensing and navigation.
High-stability inertial navigation for demanding flight conditions.
Long-duration continuity under GNSS degradation.
Stable output across thermal and vibration loads.
Machine-readable motion and attitude awareness.
06
Validation evidence across environment, navigation and lifecycle requirements.
Attitude precision and continuity by validated configuration.
Temperature, vibration and aerospace testing.
Reference kits, interfaces and deployment support.
07
Adjacent deployments with similar operating constraints.