CargoLogic

Load Sync

Mass Displacement Mapping. Measuring the impact of gravitational force on the vehicle's suspension geometry. The Oat monitors the "Payload Constant" to maintain structural integrity and kinetic balance.

• ⚖️ Metric: Cargo Load Mass (kg/lbs).
• 📐 Variable: Vertical Center of Gravity.
• 🛑 Factor: Maximum Payload Sync.

Stress Sync

Mechanical Tension Mapping. Measuring the displacement of the dampening matrix under dynamic impulse. The Oat monitors the "Elastic Limit" to prevent structural fatigue and chassis oscillation.

• 🔩 Metric: Dynamic Load Factor (%).
• 📏 Variable: Vertical Travel Displacement.
• ⚠️ Factor: Spring Rate Constant ($k$).

Optimal Sync

Mechanical Equilibrium. All suspension components operating within their primary design envelope. The Oat monitors the "Ride-Height Constant" to confirm zero structural fatigue and perfect geometry sync.

• 💎 Status: Nominal Load Distribution.
• 🌀 Damping: Critical Oscillation Control.
• 📐 Alignment: Static Geometry Locked.

Heavy Sync

High-Mass Displacement. Suspension matrix is operating near its elastic threshold. The Oat monitors the "Compression Delta" to warn of reduced dampening efficiency and increased thermal brake load.

• 🚧 Status: 60-90% Payload Saturation.
• 🛑 Braking: Extended Kinetic Dissipation.
• 📉 Travel: Minimum Rebound Clearance.

Overload Sync

System Limit Breach. Displacement has exceeded the structural capacity of the chassis and suspension. The Oat monitors the "Failure Constant" to issue a terminal warning against kinetic operation.

• 🚫 Status: > 100% GVWR Capacity.
• ⚠️ Condition: Bump Stop Contact (Zero Travel).
• 🚨 Risk: Chassis Fracture / Brake Failure.