Matched Array Flight Alignment System for Variable Control
Find Innovative SolutionsGenerate Solutions
Solution Overview
Problem
Operational systems, such as chemical processes and aircraft flight, require precise alignment of multiple variables to achieve desired outcomes, which is often challenging due to the need for human expertise and continuous evaluation of differently measured variables, leading to potential failures or accidents.
Innovation Solution
A matched array system and method that displays the interaction of two variables in a two-dimensional array, using proxy values to represent feasible ranges, allowing for visualization of optimal settings along an alignment vector, and providing audible warnings and instructions to adjust variables for optimal performance, either manually or automatically.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If human operators continuously evaluate and align multiple variables using expertise and experience, then system performance can be optimized, but the complexity of operation increases and the risk of human error remains
Solution Approach 1:
The patent introduces an alignment computer as an intermediary device that receives data from multiple sensors, processes the information, and generates alignment indicators. This mediator handles the complex task of evaluating multiple variables simultaneously, reducing the cognitive burden on pilots while maintaining reliable performance monitoring.
Solution Approach 2:
The system provides continuous feedback through alignment indicators that show whether the aircraft is in the desired flight regime. The audible warnings and visual displays give immediate feedback about variable alignment, allowing operators to make quick adjustments without needing to mentally process all the raw sensor data.
2Measurement precision
If multiple differently-measured variables are monitored on separate gauges, then measurement precision is maintained, but the difficulty of detecting and measuring alignment increases
Solution Approach 1:
The patent combines multiple separately-measured variables (airspeed, angle of attack, thrust, etc.) into a unified alignment display. The alignment computer integrates data from various sensors and presents them as a cohesive visual indicator showing whether all variables are properly aligned, making it easy to detect overall alignment without losing the precision of individual measurements.
Solution Approach 2:
The system transforms the detection problem from a two-dimensional task (reading multiple separate gauges) to a one-dimensional task (checking a single alignment indicator). By projecting the alignment state onto a single visual dimension, the system maintains measurement precision while dramatically simplifying the detection of whether variables are properly aligned.
3Adaptability or versatility
If pilots rely on measurement, experience, or feel to keep variables within operational parameters, then operational flexibility is maintained, but the loss of time for continuous evaluation increases
Solution Approach 1:
The alignment computer performs preliminary evaluation of all flight variables continuously in the background, so that when the pilot needs to make a decision, the alignment status is already determined and displayed. This preliminary processing eliminates the need for pilots to spend time evaluating multiple variables during critical moments, while the system remains adaptable to changing flight conditions.
Solution Approach 2:
The system serves itself by automatically monitoring and evaluating all flight parameters without requiring active pilot intervention. The alignment computer continuously processes sensor data and updates the alignment display, allowing pilots to focus on decision-making while the system handles the time-consuming evaluation task autonomously.
Data Source
AI summary
A matched array technology system and method for displaying in a two-dimensional array the structured interaction between different parameters of an aircraft flight. Specific applications effectively support improved flight safety and greater fuel efficiency. Proxy values of flight metrics are defined and scaled so the axes of the array contain corresponding indicators resulting in a matched array and an embedded, unique alignment vector showing the relationships between different flight variables. The flight alignment system may be used with flight data that contain discontinuities and nonlinear reversions. Wherever values intersect, flight alignment system indicators can depict proximity to the alignment vector, as well as the direction and extent of adjustments to either or both selected flight metrics to achieve and maintain controlled flight.