Redundant Piloting Sensor Device for Aircraft Ground Speed Integrity
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Solution Overview
Problem
Current GNSS systems for aircraft piloting face limitations in integrity, availability, and accuracy, especially when multiple satellites fail, and existing hybrid systems rely on a single GNSS system, leading to high costs and complexity in managing failure configurations.
Innovation Solution
A redundant piloting sensor device utilizing multiple independent GNSS systems, fault detection and exclusion modules, and inertial measurement units to determine aircraft ground speed with high integrity and availability, including multiple FDE modules for single and multiple satellite failure detection and exclusion, and hybridizing inertial measurements for continuous speed estimation.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If a single GNSS system is used for aircraft piloting, then the device complexity is reduced, but the reliability and integrity of navigation information deteriorate due to potential simultaneous satellite failures
Solution Approach 1:
The patent segments the navigation system into multiple independent GNSS receivers (at least two receivers from the same or different constellations) instead of relying on a single receiver. Each receiver independently processes satellite signals, and their results are combined through a fusion algorithm. This segmentation provides redundancy so that if one receiver or its satellites fail, the other receiver(s) can maintain navigation integrity, thereby improving reliability without requiring an overly complex centralized failure management system.
Solution Approach 2:
The patent changes the parameter of system configuration from single-receiver to multi-receiver architecture. By introducing additional receivers and combining their outputs through weighted fusion algorithms, the system transforms the reliability characteristic without proportionally increasing complexity, as the fusion process systematically handles multiple failure configurations through mathematical combination rather than exhaustive error checking.
2Reliability
If multiple independent GNSS systems are used to overcome satellite failures, then the reliability improves, but the device complexity increases due to multiple receivers and failure management
Solution Approach 1:
The patent merges the outputs of multiple GNSS receivers through a fusion algorithm that combines position and velocity information from each receiver. Instead of maintaining separate failure detection systems for each receiver (which would multiply complexity), the system combines their results using weighted averaging or other fusion techniques. This merging approach maintains high availability by utilizing multiple receivers while controlling complexity through a unified processing framework rather than multiple independent estimation systems.
Solution Approach 2:
The patent implements a universal fusion algorithm that handles multiple failure configurations simultaneously. Rather than creating specific estimators for each possible failure scenario (single satellite failure, multiple satellite failures, receiver failures), the fusion algorithm universally processes inputs from multiple receivers and naturally handles various failure modes through its mathematical structure. This multi-functional approach improves availability while avoiding the combinatorial explosion of specialized estimators.
3Measurement precision
If a hybrid system with multiple estimators is used to detect satellite failures, then the measurement precision improves, but the device complexity and cost increase significantly
Solution Approach 1:
The patent uses multiple GNSS receivers as redundant copies of the same measurement function. Instead of using a single receiver with multiple complex estimators trying to detect failures, the system deploys multiple receivers that independently perform the same position and velocity measurements. The fusion algorithm then combines these duplicate measurements, achieving high precision through redundancy rather than through multiple estimators analyzing a single receiver's data. This copying approach reduces complexity while maintaining or improving measurement accuracy.
Data Source
AI summary
A device of piloting sensors for a rotary wing aircraft having at least two IMU inertial modules, at least two GNSS receivers having respective first fault detection and exclusion modules for detecting and excluding failures and covering distinct GNSS satellite navigation systems, at least two second FDE modules, at least two hybridizing platforms, and at least one third FDE module. The FDE modules enable signals that are of integrity and/or signals that are erroneous to be detected so as to exclude each GNSS system that is defective. In addition, each hybridizing platform makes it possible to determine a hybridized ground speed in order to delivering a ground speed for said aircraft that is accurate and of integrity.


