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.
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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.
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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.
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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 Kit05
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.
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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.
