Flight Controller Boundary Enforcement for Pilot-Limited Aircraft Maneuvers
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Solution Overview
Problem
Current systems lack the capability to accurately determine and maintain aircraft flight boundaries, considering various factors such as pilot experience and environmental conditions, which can lead to unsafe flight operations.
Innovation Solution
A flight controller system that receives flight data, determines flight boundaries, sets movement limits, and generates control signals to ensure the aircraft remains within those boundaries, taking into account pilot instructions and real-time data for safe operation.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If a flight controller system is implemented to determine and enforce flight boundaries, then aircraft safety is improved, but device complexity increases
Solution Approach 1:
The flight controller is designed to perform multiple functions: receiving flight data from various sources, determining flight boundaries, setting movement limits, and generating control signals. This multi-functional approach consolidates what could be separate systems into a single integrated controller, improving safety while managing complexity through functional integration
Solution Approach 2:
The system continuously receives flight data, compares current aircraft state against determined flight boundaries, and generates control signals to maintain compliance. This closed-loop feedback mechanism ensures safety by constantly monitoring and adjusting aircraft behavior, while the automated nature of the feedback reduces the need for complex manual intervention systems
2Adaptability or versatility
If flight boundaries are dynamically updated during flight, then adaptability is improved, but measurement precision requirements increase
Solution Approach 1:
The flight boundary determination is designed to be dynamic rather than static. The controller can update flight boundaries during flight based on changing conditions such as environmental factors or mission requirements. This dynamic capability allows the system to adapt to varying operational contexts while maintaining precise boundary enforcement through continuous calculation and updating of movement limits
Solution Approach 2:
The system determines and sets flight boundaries and movement limits in advance before actual flight operations begin. This preliminary determination allows the system to prepare appropriate boundaries based on initial flight data, reducing the precision burden during actual flight by having pre-calculated reference values ready for comparison and enforcement
3Reliability
If multiple factors are considered when determining flight boundaries, then reliability is improved, but device complexity increases
Solution Approach 1:
The flight controller integrates multiple data processing functions into a single system, handling various flight data inputs and synthesizing them to determine comprehensive flight boundaries. This multi-functional design allows consideration of multiple factors without proportionally increasing overall system complexity, as the same controller handles diverse data types and decision-making processes
Solution Approach 2:
The system combines multiple data sources and consideration factors into a unified flight boundary determination process. By merging these elements into a single integrated decision-making framework rather than separate systems, the patent achieves reliable multi-factor analysis while avoiding the complexity multiplication that would result from multiple independent systems
Data Source
AI summary
A system for controlling a flight boundary of an aircraft. The system includes a flight controller communicatively connected to the aircraft. The flight controller is configured to receive a plurality of flight data linked with the aircraft, determine a flight boundary for the aircraft as a function of the plurality of flight data, set an aircraft movement limit as a function of the flight boundary, receive a pilot instruction, and generate a control signal for the aircraft as a function of the aircraft movement limit and the pilot instruction. The control signal is limits the aircraft to remain within the flight boundary. A method for controlling a flight boundary of an aircraft is also provided.