Aircraft Route Set Ranking for Multi-Constraint Airspace Planning

The patent segments the route optimization process into distinct modules: a sound propagation module that calculates acoustic impact, an aircraft kinematic module that computes fuel consumption, and a route evaluation module that integrates multiple parameters. This segmentation allows each module to be optimized independently and processed efficiently, reducing overall computational expense while maintaining comprehensive multi-parameter optimization capability.

The patent performs preliminary calculations of acoustic impact and fuel consumption for various route segments before final route determination. By pre-computing these parameters for different geographic regions and flight conditions, the system avoids redundant calculations during the final optimization phase, significantly reducing computational expense while maintaining comprehensive optimization.

The patent implements a universal route optimization framework that handles multiple parameters (acoustic impact, fuel consumption, geographic features, constraints) through a single integrated system. The sound propagation module and aircraft kinematic module serve multiple functions: they evaluate different route options, compare alternative paths, and provide input for final route selection. This multi-functionality reduces system complexity by consolidating what would otherwise require separate specialized systems for each parameter.

The patent introduces an intermediary route evaluation module that mediates between the sound propagation module, aircraft kinematic module, and final route selection. This intermediary integrates multiple parameters and constraints, transforming complex multi-parameter data into simplified route recommendations. The intermediary absorbs system complexity by providing a unified interface that manages the interaction between different optimization criteria.