Avionic Ground Station for Automated Failure Elimination
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Solution Overview
Problem
Current avionic aviation systems lack the capability for fully automated, real-time failure elimination due to technical complexity, nonlinearity in aircraft behavior, and dependence on human interaction, which leads to unpredictable operational stoppages and increased error susceptibility.
Innovation Solution
An avionic aviation system with a ground station that uses a wireless interface to activate dedicated failure deployment devices via a switching device, incorporating detection devices for takeoff and landing units, a Techlog stack for parameter logging, and a filter module to dynamically determine memory thresholds for activating failure deployment devices, allowing for automated failure elimination without human intervention.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Adaptability or versatility
If human interaction is used for failure detection and elimination, then system adaptability and judgment capability are improved, but error susceptibility and operational stoppages increase due to complexity and unpredictability
Solution Approach 1:
The system enables automated self-service through the ground station that independently monitors aircraft parameters, detects failures, and activates deployment devices without human intervention. The ground station processes sensor data, determines failure conditions, and triggers appropriate responses automatically, eliminating human error while maintaining system adaptability through intelligent algorithms.
Solution Approach 2:
The patent replaces human mechanical interaction with an electronic automated system. The ground station uses electronic sensors, data processing, and automated switching devices to substitute human judgment and action in failure detection and elimination, thereby improving reliability while maintaining adaptability through electronic control.
2Reliability
If automation is implemented for failure elimination, then operational stoppages and human errors are reduced, but system complexity and implementation difficulty increase
Solution Approach 1:
The system is segmented into distinct functional modules: sensor units for parameter detection, communication interfaces for data transmission, processing units for failure determination, and deployment devices for failure elimination. This modular segmentation reduces overall system complexity by making each component independent and manageable while maintaining high operational reliability through automated coordination.
Solution Approach 2:
The ground station serves as an intermediary between aircraft sensors and deployment devices. It receives parameter data from aircraft, processes failure conditions, and triggers appropriate deployment devices. This intermediary role simplifies the overall system architecture by centralizing the decision-making logic and reducing direct complexity between sensors and actuators.
3Speed
If real-time parameter monitoring and automated response are implemented, then failure elimination speed is improved, but data processing complexity and computational requirements increase
Solution Approach 1:
The system performs preliminary actions by pre-programming failure determination logic and deployment protocols in the ground station. When parameters are received, the system quickly matches them against pre-established failure conditions and triggers appropriate responses. This preliminary preparation of decision logic enables rapid failure elimination while reducing real-time computational complexity.
Solution Approach 2:
The system implements real-time feedback loops where sensor parameters are continuously monitored, compared against failure thresholds, and automatically trigger deployment devices when conditions are met. This feedback mechanism enables rapid automated response to failures while maintaining manageable data processing complexity through straightforward threshold-based comparison and immediate actuation.
Data Source
AI summary
An avionic aviation system including: a ground station that is linked to an aircraft via a wireless interface; wherein the ground station includes, a receiver that receives, via a wireless interface, a transmission from a detection device integrated in avionics of the aircraft, said transmission including a parameter regarding at least one of takeoff and landing of the aircraft, and a counter module that increments a value based on the parameter regarding at least one of takeoff or landing for the aircraft.