GNSS Interruption
Satellite loss in contested or obstructed environments.
Solutions / Aerospace Navigation
Aerospace Navigation
MEMS inertial sensing, fiber-optic gyro navigation and multi-sensor fusion maintain positioning and attitude through GNSS loss, thermal cycling, vibration and electromagnetic interference.
-55 to 125 C operationGNSS-denied continuityCompact mission integration
02
Mission Challenge.
Key operating constraints that shape the solution architecture.
Thermal and Vibration Stress
Stable output is required under harsh motion and temperature.
SWaP Constraints
Compact, light and power-efficient systems are required.
03
PopperSeek Solution Stack.
A complete sensing, navigation and engineering stack.
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.
04
Recommended Products.
Mission-ready modules matched to this operating environment.
POPFOG9000
Fiber Optic Gyro Navigation System
POPTCN10000
Tightly Coupled Navigation System
POPNAV8000
GNSS / INS Navigation System
Reference Kit
Evaluation & Integration Platform
05
Technology Behind the Solution.
Core technologies supporting reliable sensing and navigation.
FOG Navigation
High-stability inertial navigation for demanding flight conditions.
Drift Suppression
Long-duration continuity under GNSS degradation.
Environmental Hardening
Stable output across thermal and vibration loads.
Embodied State Interface
Machine-readable motion and attitude awareness.
06
Proof & Validation.
Validation evidence across environment, navigation and lifecycle requirements.
Navigation Proof
Attitude precision and continuity by validated configuration.
Environmental Proof
Temperature, vibration and aerospace testing.
Integration Proof
Reference kits, interfaces and deployment support.
07
Related Cases.
Adjacent deployments with similar operating constraints.
