GNSS Interruption
Satellite loss in contested or obstructed environments.
Case / Aerospace
Satellite Attitude Support
State awareness for orbital platform subsystems.
Operating Context
What the mission needs to prove.
MEMS inertial sensing, fiber-optic gyro navigation and multi-sensor fusion maintain positioning and attitude through GNSS loss, thermal cycling, vibration and electromagnetic interference.
Thermal and Vibration Stress
Stable output is required under harsh motion and temperature.
SWaP Constraints
Compact, light and power-efficient systems are required.
Implemented Stack
From sensing hardware to field support.
The case is configured around the same deployable architecture used across the PopperSeek solution portfolio.
Sensors
IMU and FOG sensing inputs.
Navigation System
GNSS / INS and inertial navigation processing.
Fusion Algorithms
Drift suppression and state estimation.
Reference Kit
Evaluation platform for integration and testing.
Engineering Support
Validation, configuration and lifecycle support.
Engineering Proof
Validated before deployment.
Navigation Proof
Attitude precision and continuity by validated configuration.
Environmental Proof
Temperature, vibration and aerospace testing.
Integration Proof
Reference kits, interfaces and deployment support.
Recommended Products
Matched hardware for this case.
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