VTOL Air Data Calibration Using Neural Networks Near the Fuselage
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Solution Overview
Problem
Existing air data indicating arrangements in VTOL aircraft fail to provide precise air speed and altitude information for all flight configurations and conditions, necessitating costly and time-consuming design iterations and posing safety risks due to the need for precise calibration of pitot and static port placements.
Innovation Solution
An air data indicating arrangement using an artificial neural network to determine air speed and altitude in real-time from flight data, including pitot tube, static port, and additional parameters, allowing for precise calibration across various flight conditions and configurations.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Measurement precision
If traditional pitot-static systems are used to measure air speed and altitude, then the measurements are affected by air flows and turbulences around the VTOL aircraft, but placing sensors farther from the fuselage increases safety risks and costs
Solution Approach 1:
The patent replaces the traditional mechanical pitot-static measurement system with an artificial neural network-based computational system. The neural network processes multiple sensor inputs (pitot pressure, static pressure, temperature, accelerometer data, gyroscope data) to compensate for the effects of air flows and turbulences, eliminating the need to place sensors in locations optimized for mechanical measurement accuracy.
Solution Approach 2:
The patent creates a multi-functional air data indicating arrangement where a single integrated system performs multiple functions: it processes pressure data from pitot and static ports, temperature data, acceleration data, and rotational data simultaneously through the neural network to provide accurate air speed and altitude measurements regardless of sensor placement or flight conditions.
2Measurement precision
If air data indicating arrangements are calibrated for precise measurements, then measurement precision improves, but calibration becomes time-consuming and costly requiring multiple design iterations
Solution Approach 1:
The patent performs preliminary training of the artificial neural network using comprehensive flight test data covering various flight conditions, configurations, and maneuvers before actual operation. This pre-training phase establishes the neural network's ability to accurately process sensor data across all expected operating scenarios, eliminating the need for time-consuming iterative calibrations during the design process.
Solution Approach 2:
The system incorporates feedback mechanisms where the neural network continuously processes real-time sensor data and adjusts its outputs based on patterns learned during training. The system can also incorporate actual flight data to refine and update the neural network models, enabling continuous improvement without requiring complete recalibration.
3Object-affected harmful factors
If sensors are positioned closer to the fuselage for safety and cost reasons, then safety and manufacturing ease improve, but measurement precision deteriorates due to proximity to air flows and turbulences
Solution Approach 1:
The artificial neural network acts as an intermediary between the physical sensors and the air data indication system. It processes the raw sensor data from pitot ports, static ports, and other sensors, compensating for the effects of nearby air flows and turbulences through learned patterns, thereby enabling accurate measurements even when sensors are positioned close to the fuselage for safety reasons.
Data Source
AI summary
An air data indicating and calibrating arrangement and method for a vertical take-off and landing aircraft, in particular a helicopter, for providing information on an air speed of the vertical take-off and landing aircraft and for providing information on an altitude of the vertical take-off and landing aircraft are described. The vertical take-off and landing aircraft includes a pitot tube device for determining a stagnation air pressure at a position of the pitot tube device and a static port device for determining a static air pressure at a position of the static port device. The air data indicating arrangement includes an air speed and altitude determination module to determine in real-time the air speed and the altitude of the vertical take-off and landing aircraft from flight data by using a regressor obtained by training an artificial neural network with training data.


