Perception
IN PROGRESS
PHYSICAL SYSTEM
- Sensor interfaces
- Camera and inertial test inputs
- Timing and calibration
SOFTWARE SYSTEM
- Vision pipeline
- Detection and tracking
- Uncertainty handling
Antshiv Robotics is developing the software and compute foundations for autonomous sensing across biodiversity conservation, infrastructure inspection, mapping, search and rescue, public safety, and defence research.
Today we are building flight-control mathematics, simulation, onboard CPU AI, and portable compute infrastructure. Over the next two to three years, we plan to connect these components into integrated aircraft and ground systems as financing, hardware access, and field partnerships develop.
Support conservation, inspection, mapping, public safety, and reconnaissance with adaptable sensing systems.
Use compact CKE models when connectivity, power, latency, or data ownership makes remote inference impractical.
Move larger models and mission analysis onto expandable ground nodes without making basic operation depend on them.
Preserve tests, telemetry, model provenance, measurements, and field observations for the next engineering cycle.
Antsand turns structured content, data, design, and site operations into deployed web applications. CKE turns model circuits and numerical contracts into auditable C runtimes for inference and training. Both make the path from intent to execution visible instead of hiding it behind a large framework.
The same method continues into flight control: begin with quaternion mathematics, state estimation, and control algorithms, then implement and measure them in C for the processors, sensors, power limits, and aircraft Antshiv Robotics selects. Across the stack, we optimize for auditability, performance, and the engineering intuition to understand why the complete system behaves as it does.
Describe motion, sensing, uncertainty, computation, timing, energy, memory, and communication before choosing an implementation.
Separate flight safety, onboard perception, ground compute, data, and operator interaction into interfaces with known failure behaviour.
Implement control software, C kernels, model circuits, simulation, telemetry, data pipelines, and the hardware paths connecting them.
Run the system, compare it with mathematical and software references, inspect failures, and carry the measurements into the next engineering cycle.
Flight-control algorithms turn estimated state into safe action. CKE turns model circuits into auditable CPU execution for inference and training. Expandable CPU nodes provide additional memory and compute, while Antsand organizes the interfaces, evidence, telemetry, content, and operational records around the work.
CKE provides the AI execution layer inside the larger Antshiv system. It connects model structure to explicit circuits, generated C, native CPU kernels, and evidence we can inspect.
Equation → model → numerical contract → kernel or controller → native execution → hardware behaviour → measurement.
A C-first compiler and runtime that turns model weights and circuit templates into inspectable generated C and native CPU kernels.
Rigid-body mathematics, state estimation, simulation, and sensor fusion built methodically toward controlled autonomous systems.
Structured experiments, telemetry, evidence dashboards, deployment tooling, and technical publishing that preserve the reasoning behind each result.
Antshiv Robotics is bringing its flight-control, CPU AI, and systems work together as one long-term aircraft programme. The flight computer handles stability and recovery, CKE adds onboard perception, and portable CPU nodes provide larger models and mission analysis when a network connection is available.
This is a two-to-three-year development direction. Current investment is concentrated on the software layer and expandable CPU nodes. Aircraft integration follows as financing, hardware access, and test partnerships allow us to move from simulation into hardware-in-the-loop and relevant-environment testing.
Stabilization, state estimation, navigation, geofencing, return-to-home, and emergency recovery belong to the deterministic flight computer. This gives the aircraft a reliable operating foundation before additional AI capabilities are introduced.
A power-bounded companion computer runs selected vision, audio, or language circuits for perception and decision support. A model crash or missed deadline cannot take ownership of the safety loop.
Expandable CPU nodes provide more memory, storage, and distributed compute for mission analysis, multi-aircraft coordination, and larger models. Loss of that link reduces capability, not basic flight safety.
We will move from component tests to closed-loop simulation, hardware-in-the-loop testing, and relevant-environment trials. At each stage we will measure latency, power, communication behaviour, recovery paths, and the provenance of models and observations.
These examples link to the source code, test reports, and engineering records behind the current work.
CKE supports multiple Qwen, Gemma, GLM, Nanbeige, and multimodal paths through explicit model-family contracts.
The v8 pipeline lowers model circuits to deterministic C and rejects missing kernels, routes, or numerical contracts instead of silently falling back.
Layered scalar, ISA, and end-to-end gates compare CKE with PyTorch and llama.cpp and identify the first divergent operation.
Current work spans AVX2, AVX-VNNI, AVX-512, AMX BF16, and ARM NEON, with measured support stated separately from work still being hardened.
Rigid-body mathematics, control systems, sensor models, and reproducible simulation are being developed before any autonomous-product claim.
ShivasNotes publishes the derivations, architecture, debugging evidence, and limitations behind the work.
These are research responsibilities and maturity targets, not a claim that a finished autonomous drone is currently available.
IN PROGRESS
PHYSICAL SYSTEM
SOFTWARE SYSTEM
IN PROGRESS
PHYSICAL SYSTEM
SOFTWARE SYSTEM
IN PROGRESS
PHYSICAL SYSTEM
SOFTWARE SYSTEM
IN PROGRESS
PHYSICAL SYSTEM
SOFTWARE SYSTEM
PLANNED
PHYSICAL SYSTEM
SOFTWARE SYSTEM
PLANNED
PHYSICAL SYSTEM
SOFTWARE SYSTEM
Each article turns a code change, mathematical question, or measured failure into a durable explanation.
How model-family structure becomes explicit compiler input rather than hidden runtime convention.
How Q4_K, Q5_K, Q6_K, Q8_K, and mixed dot products move through real CPU kernels.
Why one model becomes two CPU workloads with different matrix shapes, memory traffic, and execution plans.
We take on well-scoped problems where a model, runtime, control system, or Linux CPU path is unsupported, slow, numerically wrong, or difficult to audit.
Feasibility, performance, and first-divergence analysis for CPU inference.
Runtime-versus-reference divergence localization, operation by operation.
Kernel, memory-path, portability, and profiling work on real hardware.
Robotics mathematics, deterministic simulation, and control-system prototyping.