Military satellites, re-entry vehicles, HAPS platforms, and hypersonic systems need inertial reference that performs where external signals cannot reach.
Near-space and aerospace systems operate where GPS signals are weak, plasma effects block communication, and external references are unavailable during the most critical phases of flight. Hypersonic vehicles at extreme speed degrade all signal links — the inertial core becomes the only navigation backbone.
IMS-AI delivers continuous attitude reference through re-entry, HAPS station-keeping, and hypersonic glide phases. The EKF fusion architecture rejects noise from vibration and electromagnetic environment characteristic of high-speed aerospace operation. Temperature-calibrated per unit across the full operating range.
| Architecture | Parallel MEMS array with EKF + AI fusion |
| Operation | Fully passive — no RF emissions, no signal dependency |
| Fault tolerance | Graceful degradation — no single point of failure |
| Environment | Calibrated for launch and high-speed flight regimes |
| Output | UART / SPI / CAN — compatible with standard flight stacks |
| Detailed specs | Available under NDA to qualified programs |