Navigation Instruments TRIZ Cases

Pre-calculated landmark visibility ranges in autonomous vehicle maps reduce power consumption by triggering sensor detection only within specified zones.

Automated object detection replaces manual verification of rasterized map images, resolving the contradiction between high accuracy and slow update efficiency.

Road surface evaluation apparatus adjusts driving information volume based on roughness change rates.

A routing system directs mobile sensors to hexagonal zones based on air quality variance.

A context server correlates accuracy and probability parameters to meet requested quality levels.

A map curation management system uses predictive models to estimate manual correction time and generate heat maps.

Aircraft navigation system generates virtual runway centerline using onboard inertial data and camera imagery.

A data updating device generates mesh map data using intersecting straight lines to determine update locations efficiently.

Edge indicators show points of interest outside the current map view, reducing complex zooming and panning operations.

Mission information manager filters and presents relevant flight data to support crew decision-making.

Co-located coils generate magnetic fields for position determination using invariant scalar values, eliminating expensive stable time bases.

A rotorcraft alert system overlays wind velocity and direction symbols on cockpit displays to indicate potential loss of tail rotor effectiveness zones.

A dynamic display system evaluates aircraft state variables to modify flight maps in real time.

Navigation system displays local brand icons using color differentiation schemes to indicate business categories.

A GNSS receiver qualifies satellite signals using propagation characteristics to filter invalid data before position calculation.

Automated avionics system detects functional changes and monitors pilot audio responses to ensure operational awareness.

A flight management system calculates precision parameters to determine angular guidance mode compatibility for aircraft approaches.

Color-coded flight display indicators show armed and activated states of segmented approach procedures to resolve insufficient pilot situational awareness.

A monitoring system processes ground condition and surface topography data to predict instability risks for work machines moving along a route.

Unmanned drive units navigate inventory facilities using fiducial markers with a small set of values to determine precise location.

Calibrating inertial measurements with satellite-based augmentation system positions creates corrected data for real-time monitoring.