Aircraft Speed Alert System for Restricted Airspace Compliance

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Pilots may inadvertently exceed speed limits in airspace with restrictions due to cockpit workload, highlighting the need for a method to alert aircraft of potential speed violations.

Innovation Solution

A system that retrieves an aircraft's flight plan, generates a predictive speed profile based on current position and trajectory, calculates a deceleration time window, and displays an alert to the crew when approaching speed-limited airspace to allow sufficient time to comply with speed limits.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the pilot manually monitors and complies with speed restrictions, then the aircraft can maintain speed limits, but the pilot may inadvertently forget due to cockpit workload and violate speed limits

Engineering Contradiction:
Improvespeed limit complianceVSAvoidcockpit workload
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The system enables the aircraft to monitor its own speed and automatically determine compliance with speed restrictions without requiring continuous manual pilot intervention. The Flight Management System continuously compares actual speed with restricted speed values, allowing the aircraft to self-monitor and self-report compliance status.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The system provides continuous feedback to the pilot through the display unit regarding speed compliance status. When the aircraft approaches or exceeds restricted speed, the system generates visual alerts and messages, creating a feedback loop that informs the pilot of compliance status and enables timely corrective action.

Inventive Principle:
Principle #23Feedback

2Reliability

If the system provides early alert to allow deceleration, then the aircraft can comply with speed limits, but the alert must be generated with sufficient lead time

Engineering Contradiction:
Improvespeed limit complianceVSAvoidreaction time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The system performs preliminary calculations to determine the time required for the aircraft to decelerate to compliant speed. By calculating this deceleration time in advance and providing alert accordingly, the system ensures the pilot receives warning with sufficient lead time to take corrective action before violating the speed restriction.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system dynamically adjusts the alert timing based on the aircraft's current speed, deceleration rate, and distance to the restricted airspace entry point. This dynamic calculation ensures the alert is provided at the optimal moment - early enough to allow compliance but not so early as to cause unnecessary concern.

Inventive Principle:
Principle #15Dynamics

3Reliability

If the system continuously monitors speed and generates alerts, then speed violations can be prevented, but the system complexity increases

Engineering Contradiction:
Improvespeed violation preventionVSAvoidsystem complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The system leverages the existing Flight Management System's multi-functional capabilities to perform speed monitoring, compliance determination, and alert generation. By utilizing the FMS's existing flight path management, performance data collection, and display capabilities, the system avoids adding separate dedicated hardware components.

Inventive Principle:
Principle #6Universality (Multi-functionality)

Solution Approach 2:

The speed compliance monitoring function is merged with the existing flight path management and performance monitoring functions of the Flight Management System. The same processor and sensors used for other flight parameters are utilized for speed restriction compliance, consolidating multiple functions into a single integrated system.

Inventive Principle:
Principle #5Merging (Combining)

Data Source

PatentEP3547284B1Method and system for generating an alert for an aircraft potentially exceeding speed limits in restricted airspace
Publication Date: 2022.04.20 HONEYWELL INTERNATIONAL INC
  • EP3547284B1 patent drawingFigure 1
  • EP3547284B1 patent drawingFigure 2
  • EP3547284B1 patent drawingFigure 3

AI summary

Methods and systems are provided for generating an alert for an aircraft potentially exceeding speed limits in airspace with speed limitations. The method comprises retrieving a flight plan for the aircraft and identifying airspace with speed limitations along the flight plan. A speed profile is generated based on the in-flight aircraft's current position, speed and trajectory. Any predicted speed violations are identified by comparing the speed profile with the airspace with speed limitations along the flight plan. A predictive time window is calculated that allows for the in-flight aircraft to decelerate sufficiently to comply with the speed limits of the airspace with speed limitations. The predictive time window includes a zone for the aircraft to reduce its airspeed and a reaction buffer zone to allow the aircrew sufficient time to comply with instructions to decelerate the aircraft. Finally, an alert is generated for the crew of the in-flight aircraft upon entering the predictive time window.