Avionics Wake Conflict Prediction for Intruder Aircraft Avoidance

The system performs preliminary actions by predicting the future positions of wake vortices before the subject aircraft encounters them. The processor calculates where wake vortices will be at future time points along the subject aircraft's flight path, enabling proactive avoidance rather than reactive response. This resolves the contradiction by establishing prediction capability without requiring overly complex systems, as it builds upon existing intruder detection functionality.

The patent introduces an intermediary computational layer that processes intruder aircraft data, predicts wake vortex trajectories, and generates avoidance guidance. This intermediary system acts as a mediator between raw sensor data and pilot action, automatically performing the complex calculations needed for wake avoidance while presenting simplified guidance to the pilot. This resolves the contradiction by handling complexity internally while maintaining operational simplicity.

The system applies partial action by focusing computational resources on predicting only the relevant wake vortex parameters (position, strength, size) that directly affect the subject aircraft, rather than modeling all atmospheric conditions. The processor calculates wake vortex characteristics at discrete future time points along the flight path, providing sufficient prediction accuracy without excessive computational overhead. This resolves the contradiction by achieving adequate turbulence avoidance with moderate energy consumption.

The system utilizes existing aircraft systems and data sources (intruder detection device, flight path information, aircraft performance data) to generate wake predictions, rather than requiring entirely new sensing or measurement capabilities. The processor leverages data already available on modern aircraft, performing self-service through intelligent computation of wake parameters from existing operational data. This resolves the contradiction by reducing additional energy requirements while maintaining effective turbulence avoidance.

The system implements feedback by continuously monitoring the subject aircraft's flight path, intruder aircraft positions, and wake vortex predictions, then adjusting avoidance guidance based on changing conditions. The processor recalculates wake vortex positions and recommended avoidance maneuvers in real-time, providing ongoing feedback to the pilot. This resolves the contradiction by maintaining pilot authority while enhancing safety through continuous automated monitoring and adaptive guidance that responds to dynamic flight conditions.

The system provides preliminary avoidance guidance to the pilot before wake conflicts become critical, allowing the pilot to take corrective action while maintaining full control authority. Rather than automated强制执行 maneuvers, the system calculates and presents avoidance options in advance, enabling the pilot to make informed decisions. This resolves the contradiction by enhancing safety through early warning and guidance while preserving pilot decision-making authority and control.