ETTC

Abstracts

KEYNOTES

Flight tests and instrumentation in the airdrop field within the French MoD

Basile Perrin

DGA Aerospace Systems

Kineis is in the air, IOT everywhere

Céline Loisel

KINEIS

RACER high speed rotorcraft demonstrator:  innovation in numerous technical domains including Flight Test Installation

Dominique Fournier, Marc Seznec

Airbus Helicopter

Hydrogen Electric Business Jet Development

Matthieu Pettes Duler

Beyond Aero

 IRIS²: The secure connectivity constellation

Jean Pierre Diris

CNES 

Cleansky 2 D08 Distributed Electric Propulsion – Scaled Flight Demonstrator DEP-SFD : From the idea to in-flight demonstrations derisking differential thrust for flight control

Carsten DÖLL

ONERA

CONFERENCE PROGRAM

HYBRID TESTING

Integration of a Hybrid Electric Turboprop into a Powerplant Bench

Santiago Rafael López Gordo, Baptiste Jouy and Jean-Michel Bazet – Airbus Defence And Space / Safran Helicopter Engines

In the field of aerospace testing, one of the most impressive lab test means is a Powerplant bench, if it is considered a hybrid thermal electrical Powerplant, then the impression is even higher.

Clean Aviation project, promoted by the European Union, has the objective of transforming the future of civil aviation into a more efficient and sustainable industry, by considering new technologies, oriented to electrical and hybrid aircrafts, in order to ensure 30% greenhouse emission reductions by 2030, with the aim of a technology maturation toward Entry Into Service by 2035.

Through HE-ART project, Clean Aviation sponsor the evaluation of an eTP (Hybrid Electric Turboprop) designed for aircraft use, at which propulsion big players such as Rolls Royce, Safran and Ratier Figeac are collaborating with airframers such as ATR, Leonardo, Airbus Helicopters and Airbus Defence and Space.

The eTP solution merges a fuel turbine with a high voltage drive train to provide an efficient propeller demonstrator whose objectives are to ensure the safety integration of the powerplant (electrical and thermal drive train); high voltage electrical network and protections integration at nacelle; heat management characterization for future nacelle development; engine mounting system validation.

To fulfil these objectives, in its powerplant bench, Safran challenging task is to provide a real time solution to integrate a wide variety of sensors and modules coming from each project partner for various needs: engineering and TRL maturation, Real Time monitoring for safety, control of the eTP… An example of this is the telemetry of the propeller for a safety operation in the test bench.

This paper will explain the integration carried out in the Powerplant bench, the instrumentation organisation decided and the testing to be provided on to the bench for developing Hybrid Electrical technologies.

Leveraging ED-247 and DDS as Enablers for Hybrid Test Benches in the Cloud

Soeren Reglitz, Jan Wasmund and Malte Grochow – dSPACE GmbH

The computational effort required to simulate a complex cyber-physical system of systems often exceeds the available resources of a single computing node. Therefore, running these simulations in a cloud environment has become increasingly important to dynamically scale the required resources and enable early parallel testing in a virtual environment. However, as the target hardware becomes successively available for the different subsystems in later development phases, it is then necessary to couple virtual simulations with physical devices. This paper describes a novel approach how to realize the coupling between a software-in-the-loop (SIL) simulator running in a cloud environment (Kubernetes) and a hardware-in-the-loop (HIL) simulator connected to the physical device under test (DUT). In such a hybrid setup, one of the most challenging tasks is setting up the communication. This includes communication between the SIL simulators running in the cloud, as well as between the SIL simulators and the HIL simulators outside the cloud environment. Signals and buses need to be virtualized to establish communication between the SIL and HIL simulators forming the hybrid test bench. For this purpose, EUROCAE standard ED-247 revision A is used, also known as VISTAS, defining a UDP-based protocol for the virtualization of signals and buses in the aerospace domain. However, ED-247 revision A was not specified with a cloud use case in mind. Specifically, the need to define a static IP configuration for ED-247 participants makes it difficult to use in the cloud. This paper describes a solution for this issue by explaining how to realize hybrid communication between an ED-247 Virtual Component (SIL) and an ED-247 Bridge Component (HIL) using a Data Distribution Service (DDS) implementation as middleware. By wrapping the ED-247 communication in DDS and using a DDS Cloud Discovery Service in the cloud, this approach enables the ED-247 communication between multiple virtual and bridge components, both in the cloud and on-site, thus offering a flexible means of setting up the test environment according to changing needs in different development phases.

Distributed Testing – ED-247 and beyond

Ramiro Rodriguez – Airbus Helicopter

Virtualization protocols like EUROCAE ED-247 and VPNs like IPsecV2 provide extended possibilities for designing future test benches architectures but also redefining test strategies. As the standard is more largely accepted and promoted, COTS equipment become available simplifying the setup and implementation of this technology for new or existing rigs.

We presented in 2022 some Proves of Concept of different setups where these technologies could be used to interconnect benches in different locations in a simple and non-intrusive way.

Since then, Airbus Helicopters has deployed these solutions in several real use cases, including transcontinental connections and wireless connectivity systems with success but with its related number of difficulties and challenges. This year we will be presenting those results and the implemented solutions to overcome encountered difficulties and blocking points.

SENSORS

Assessment of piezoelectric strain gages in space industry

Noellie Chauvet, Etienne Cavro and Jean-Sébastien Moulet – Airbus Defence & Space / Worms Sensing

During vibration testing the common practice is to follow the structure dynamic behaviour via accelerometers but also strain gages to measure and/or monitor the deformations applied.
In the context of space industry, strain gages are used as a complement to accelerometers to instrument a specimen for dynamic tests (vibrations, shocks, acoustics) and thus estimate stresses at some specific locations of the structure or in rods. The preparation and installation of classical strain gages requires a certain know-how and their post-processing or analysis is not often so easy.

Strain gages are sensors commonly used in order to measure a structure deformation during mechanical or thermal cycling tests. A “classical” strain gage is composed of a metallic wire which deforms under an applied stress, which induces a variation of its resistance, this resistance being a function of the deformation undergone. However, the resistance values measured are too low to be directly detected and it is necessary to mount a Wheastone bridge and to follow the variations of tension. In this context the signals are generally quite noisy and difficult to post-process and analyse, in particular in the frequency and amplitude ranges applicable to space industry.

New technical solutions based on piezoelectric strain gages have recently emerged, in particular thanks to the company Wormsensing which develops two versions: a passive one and an IEPE one (Integrated Electronics Piezo-Electric), both of them being also available in a longer size. Installation, connection and handling of these strain gages are then significantly eased and quickened compared to a “classical” strain gage.

A large dynamic tests campaign (swept sine, random, transient on shaker, acoustic tests) has been carried out in order to assess the performances of these new piezoelectric strain gages in comparison to the classical ones, with a focus on the IEPE version. The measurement quality has also been compared to the one of accelerometers commonly used for dynamic tests.

The results obtained from various tests are presented here along with an assessment of the performances of these piezoelectric strain gages and the main steps of the way forward for their use and adaptation to the space context.

Optimization of Mechanical Test Preparations

Noellie Chauvet, Mathilde Cauhope, Luc Dehez and Julien Godeau – Airbus Defence & Space

Airbus Defence & Space EVT (Toulouse) conducts several dozen mechanical test campaigns (Vibration, Acoustic, Shocks) each month, requiring several dozen to several hundred measurement channels.

A test campaign generally takes place over several runs of a few minutes, while the preparation can take several days.

To reduce this preparation phase and improve competitiveness, the sensor management tool GesCAO coupled with the acquisition preparation tool DynaPrépa have been developed around the DynaWorks solution.

In 2024, this suite was completed with the tablet app StickAssist to ensure digital continuity and eliminate paper during the bonding phase.

Revolutionizing Vibration Measurement: A Breakthrough in Strain Sensing Technology

Catherine Cadieux and Houssam Yousfi – Wormsensing

For decades, accelerometers have been the cornerstone of vibration measurement in both laboratory and industrial settings. However, while strain is a critical metric directly linked to force, stress, and fatigue failure, its practical assessment has limited its widespread adoption. Wormsensing has now overcome these limitations with a groundbreaking innovation: Dragonfly® a sensor based on a 2D flexible piezoelectric crystal. This transformative technology enables strain measurement with a resolution 1,000 times greater than conventional methods, unlocking previously inaccessible frequency ranges and magnitudes.

The Dragonfly® sensor sets a new standard in vibration measurement, offering an unparalleled bandwidth of 0.01 Hz to >100 kHz and a dynamic strain range of 0.005 to 3,000 µm/m with no power consumption. This breakthrough opens exciting possibilities for advanced industrial monitoring and cutting-edge laboratory research.

This presentation will introduce the novel sensor concept and explore its transformative applications in two key areas transposable to the aerospace-industry:

  1. Strain for Force Measurement: By retrofitting the Dragonfly® sensor, 3D forces on machine tools can now be measured with unprecedented precision. This innovation redefines standard monitoring practices in the machine-tool industry, providing a metric directly tied to machine and process failure, enabling predictive maintenance and enhanced operational efficiency. Application case related to aerospace presented in detail in the submitted paper ‘’Assessment of piezoelectric strain gages in space industry’’ by Chauvet et all.
  2. Strain for Machine Diagnosis: Traditional diagnostics for rotating machinery, based on acceleration, fall short at low rotational speeds. The Dragonfly® sensor leverages dynamic strain to measure whip and whirl in motor-generators, offering new diagnostic capabilities that were previously unattainable. This advancement promises to revolutionize the field of rotating machinery diagnostics.
Capacitive solutions for the new challenges of the Aeronautics industry

Daniel Leroy and Alain Bruère – Alliantech

  • SHM: Predictive maintenance for engines
  • Performance of new fuels
  • Dynamic humidity measurement

TEST DATA ACQUISITION, NETWORK AND RECORDING

Managing the obsolescence of a critical FTI system for in-flight configuration modification

Roberto de Nardi, Eric Walker and Nicolas Cholet – Airbus Operations

Testing the various configurations of Avionic Computers on ground and in flight is one of the missions of the Flight Test Installation. In this context, the ADIS (AFDX Digital Injection System) equipment allows to retrieve internal parameters normally hidden and to modify the configuration through constraints, variables and signals in flight. It is principally used to tune the flight control laws and it’s the only intrusive FTI equipment. The new version of the ADIS needs to be more easily integrated into the FTI and the normal installation of the A/C. And also versatile on each program or platform. Through rigorous testing and validation, the new FTI system offers a more robust and future-proof solution for in-flight testing, ensuring both operational continuity and adaptability for actual and future aviation requirements. It’s in the continuity of the SKYbox FTI, the new product line.

Partial discharge testing on inverter-fed electrical machines using high repetition rate excitation source up to 1 khz

Federico Rosignoli, Enrico Concettoni, Alessandro De Grassi and Andrea Cavallini  – Loccioni / Dept. of Electrical, Electronic and Information Engineering « Guglielmo Marconi »

In inverter drives, the electrical machine insulation is subjected to high voltage stresses. If the voltage stress exceeds the Repetitive Partial Discharge Inception Voltage (RPDIV), premature failure of the stator insulation is likely to occur. Untimely failures are especially feared in e-mobility applications due to the widespread use of SiC power modules (which exacerbate the voltage stress) and safety issues. E-mobility applications include a fortiori, aircraft electrical drives, where low air pressure can cause a notable reduction of the RPDIV (about 50%).

To assess the quality of the insulation during factory acceptance tests, it is very important to mimic the voltage stress in operation. Historically surge voltage testers are used. These devices work at 10 Hz or similar, and their voltage waveforms significantly depart from those produced by an inverter. As a results, the different parts of the insulations might not be tested as expected. Due to the similarity with inverter voltage waveforms, square wave high repetition rate (SWHRR) voltage sources are the best choice to mimic the voltage stress in operation.

A setup able to excite the windings with variable rise time and pulse width (1 to 5 us) with a repetition rate up to 1 kHz is presented. An acquisition system composed of a RF antenna and a specific acquisition system is used to acquire the signal related to the occurrences of partial discharges. All bench setup is checked, using a passive dummy, to be a PD free system up to 6kV; the tests are performed inside a shielded enclosure that avoids the influence of environmental noise on the measurements. The signal is processed to improve the signal-to-noise ratio and derive the value of RPDIV.

A comparison of results between the different parameters is shown: using the SWHRR decreases the cycle time and increases the repeatability of RPDIV measurement. Considerations on the feasibility of testing stators of actuators to be used in aircraft applications will be reported.

Data evaluation of different data streams from a helicopter wind tunnel test

Erik Brehl and Oliver Schneider  –  DLR

Within one of the DLR guiding concepts “The Rescue Helicopter 2030” a new medium size helicopter wind tunnel model was designed, manufactured, and tested in two wind tunnel test campaigns. The first test was conducted in 2020 with a basic model setup without rotor blades. For this campaign the model was equipped with instrumentation in the non-rotating domain only without rotational sensors. The aerodynamic properties of two different fuselages were measured. The reference-configuration

represents the state-of-the-art fuselage comparable to the Airbus Helicopter EC135. Furthermore, an optimized design for a conventional rescue helicopter was tested. In 2024 the model was completed with further instrumentation and a complete main rotor system. The model instrumentation of the fixed system contains a 6-component main balance for the rotor system, a separated 6-component fuselage balance, three 3-axis accelerometers, pressure sensors (static & dynamic) and additional six channels for a stabilizer balance or wings. These non-rotating sensor data were collected by the TEDAS 3 Data Acquisition System. The wireless Data Acquisition System was completed and installed in the rotational model part on top of the rotor head. A new set of rotor blades was manufactured in-house. These carbon rotor blades were equipped with strain gauges (flap, lag, torsion) and dynamic pressure sensors. Sensors for blade pitch angle and pitch link force measurement were installed as well. Two wings were designed and manufactured, which could be mounted optionally at the main model structure with dedicated 5-component wing balances. The non-rotational data were acquired in a rotor triggered acquisition mode with a continuous data stream. The rotational data acquisition was based on a fixed clock with a fixed sample block length. Both streams include a time stamp and an analog sensor signal (1P) from the rotor azimuth position. Based on this azimuth position the data streams can be synchronized and the influences of the rotor to the fuselage can be investigated for different trim settings. The following paper describes the data evaluation of the data streams collected by the rotational and non-rotational Data Acquisition Systems.

Designing A User Experience (UX) for Encryption Key Loading

Malcolm Weir – Ampex Data Systems Corporation

Data-at-Rest Encryption is now generally mandated in some form or other for most new systems (as well as many established ones). While there are a few different approaches to implementing the encryption mechanism(s), there are vastly more issues involved in deciding how the keys get loaded into the system for use. Understandably, security authorities are often unwilling to share the specifics of a given approach for a given platform, but there are several common concepts that may apply when considering what might be appropriate for a new system. However, there is no universal key loading interface, nor is one likely to be appropriate. The latest NATO Advanced Data Storage Interface (NADSI / STANAG 4575) has had to address the lack of this universal method, and is used as an example of how any user experience / user interface can be accommodated.

Facilitating Advanced Real-Time Data Processing Through Auto-Coding: An Application of Large Language Models for Intelligent Flight Test Instrumentation

Arthur Mourgue, Ghislain Guerrero, Rémy Pelluault and Quentin Lecoq – Safran Data Systems

In Flight Test Instrumentation (FTI), data has always been the cornerstone of success, continuously in high demand. The advantages are clear: more data facilitates the creation of accurate digital twin models, thereby accelerating development and testing cycles necessary for certification.

Data is stored on-board and transmitted to the ground via telemetry, despite bandwidth limitations that can be mitigated through on-board processing to extract meaningful information from the acquired data. However, to maximize its utility, instrumentation engineers now must program these on-board computers to cater to their specific FTI requirements.

Nowadays, innovative solutions based on Artificial Intelligence (AI) have emerged from the mass market, revolutionizing our interaction with technology. Large Language Models (LLMs) have ushered in a new era, becoming an integral part of the web’s infrastructure. These powerful models have transformed traditional use cases, enabling document summarization, image generation, and even code generation and review.

Thus, how can we harness these new tools to address the specific needs of FTI?

This paper presents the results of an experiment conducted by Safran Data Systems, aimed at facilitating user-defined on-board processing by leveraging cutting-edge technologies while avoiding potential pitfalls.

ASPID (advance streaming protocol interface device)

Antonio Jimenez Duro, Ignacio Casillas Perez, Pilar Vicaria Torralbo, Alejandro Beloso Villar and Joaquin Pablos Palomino – AIrbus Defence & Space Spain

Digital data distribution systems in Aerospace and Defense facilitate device communication, often requiring monitoring of data traffic for Flight Test Instrumentation (FTI). The number of aircraft systems that use

Ethernet communication has increased greatly in recent times, making this type of device necessary for flight testing.

This paper discusses the use of ASPID network taps, which enable ethernet network access without additional FTI systems. ASPID taps include Inline Network Taps and end-point taps, supporting various functions. Inline Taps pass data while copying it to mirror ports for analysis.Key features include modular design, MEMS relay technology for power failure resilience, automatic port configuration, timestamp insertion, IENA headers,data filtering and configurable CBIT Outputs. These advanced capabilities are crucial for monitoring critical ethernet network segments in FTI applications.

Enhancing Structural Health Monitoring data acquisition while ensuring compatibility with existing systems

Patrick Quinn, Manuel Jesus Justicia Alados, Jaime García Alonso and Natalia Esteve Ferrer – Curtiss Wright / Airbus Defense & Space

Operational Monitoring Structural Health Monitoring (SHM) systems fulfil Fatigue Monitoring purposes of in-service aircraft. The deployment of this technology on Airbus’ fleet helps identifying potential issues before they happen. This paper discusses the use case and techniques enhancing the Operational SHM on-board data acquisition providing Damage Monitoring capabilities, in particular event diagnosis (i.e., mechanical impacts diagnosis). Specifically, gathering data from accelerometers and Piezoelectric sensors, acquired via high-speed acquisition cards able to maintain compatibility with the existing Operational SHM systems on-board and providing diagnosis information about events that could potentially affect the structural integrity of the aircraft.

Lesswire architecture in Flight Test Installation: the best compromise for easy installation and minimum operating constraints

Rémi Calin and David Cumer – Airbus Operations SAS

Systems installed in aircraft are more and more dense and compact. Available volumes are reducing. That’s why installation of acquisition devices and sensors is often a headache !

Thanks to miniaturised electronics pushed by the smartphone and automotive industry, systems used in FTI are getting smaller and smaller. Using this technology, our Flight Test Installation have reduced his footprint thanks to Remote Acquisition Unit that have replaced the traditional centralized acquisition in cabin and improve significantlty the size of the harnesses.

Unfortunately, we always face challenge for installing our FTI. Even with small devices, wiring must be improved and optimised.

To solve this issue, we have been using since many years a daisychain architecture approach based on Power Over Ethernet principle giving low intrusivity before pushing for wireless mature solutions.

This paper details the benefits for using this kind of solution that is a very good compromise to simplify installation, to integrate new systems and to minimise operational constraints.

able CBIT Outputs. These advanced capabilities are crucial for monitoring critical ethernet network segments in FTI applications.

VIDEO

A car LIDAR to measure wing bending in flight

Israel López Herreros, Felix Arévalo Lozano and Jesús Barrera Rodríguez – Airbus Defence & Space Spain

In the field of aerospace testing, extensometers and photogrammetry are two traditional technologies used to measure deformations in components such as aircraft wings or other structures, providing valuable data for structural design. However, the cost of integrating extensometers into an aircraft can be very high.

Car LIDAR-based techniques emerge as promising alternatives for improving safety and autonomy. The current challenge is to assess a car LIDAR as a flight-testing technology less intrusive and more operationally efficient to measure the flexion and torsion of a wing. According to our estimates processing with this sensor costs half as much as processing with photogrammetry.

Simulation and ground tests on a wing mockup were used to validate the methodology. This work was presented at the ETTC 2024. This paper will explain the assessment of using a LIDAR to measure the wing bending in flight. Fusion with camera images and clustering algorithms will be fundamental elements of this process. Lessons learnt and results from flight testing will be presented in this paper.

Video Compression Optimization for Telemetry Applications

Stephen Schaphorst and George Nelson – Delta Digital Video

Video compression and transport methods are critical components of a video telemetry system. Meeting video quality, resolution, frame rate, latency, and interoperability requirements can be a challenge when up against datalink bandwidth and platform SWaP-C constraints. A range of video compression and transport options is presented, from highly compressed (H.265), to medium (JPEG 2000), light (JPEG XS), and lossless compression, as well as uncompressed (SMPTE 2110-20) networked architectures. The benefits and disadvantages of the different options are described, along with real-time datalink, ground network video distribution, and video recording use cases.

 

Image Comparison From Challenges To Solutions

Fabien Meslet-Millet, François Lefebvre-Albaret and Adil Soubki – Airbus Operations

Image comparison is a recurrent task, with a high added value, involved in heterogeneous domains. The spectrum can go from checking the conformity of samples from aircraft paint (visual inspection) to compare the rendering of a system on a screen (visual comparison). Nowadays, the process mainly involves humans and his variability which depend on psychological and environmental factors. Despite the variety of missions, we identified a common set up for image comparison. In this paper, we will provide a generic approach to bring solutions to automate the actual costly challenges of image comparison. This approach will cover the usage of traditional image processing techniques to more advanced Artificial Intelligence (A.I.) solutions.

METHOD & TOOLS

A PostgreSQL-Based Tool for Locating Flight Test Conditions with Indexing Optimization

Sergio Penna and Thiago Reis – Instituto Superior de Engenharia do Porto / EMBRAER

This article presents a tool designed to locate flight conditions based on data from previous flight tests. By leveraging advanced indexing and search capabilities, this tool empowers engineers to query and analyze historical data before requesting new flight tests, thus avoiding redundant flight tests in future campaigns. Furthermore, engineers will be able to find abnormal sensor behaviors and even monitor them throughout the Flight Test Campaign.

MILESTONE - Wide Range Ability Data Acquisition Software

Bartosz Pawelczyk  Airbus Helicopters Poland

In many tests the appropriate software playsa significant role. It should assure for acquiring data from a wide range of the measurement hardware, monitoring data for any values exceeding, as well as logging data for late postprocessing and analysis. A suitable software allows to perform many sorts of tests with usage of the data acquisition system for stationary domain measurement, as well as for rotational domain measurement such as telemetry systems. Furthermore, such software should allow using the mentioned types of hardware in different configurations with the measurement syncing support through the local network.

 In this article, there is the presentation that exemplifies such software and uses its capabilities during the real test campaign. The MILESTONE software was created in order to standardize the testing process and fulfill many requirements such as: reduction time of the data acquisition system preparation, simplification and speed up of configuration, ability to communicate with the NI-cDAQ series measurement cards and other measurement systems utilizing IENA (Installation d’Essai Nouveaux Avions) protocol including FTI Flight Test Instrumentation) telemetry systems, data recording to compatible with post-processing software format file, ensuring safety during test by the limits monitoring and taking action such as warnings, permission to start or emergency stop the test bench and transmitting data through the IENA protocol for the measurement visualization purpose. A versatile and flexible software MILESTONE can cope with the most complex and demanding tests.

Interactive, persistent, and scriptable big-data visualization in the web

Philipp Grüber – Airbus Defence and Space GmbH

Modern test aircraft generate an ever-increasing amount of data that often needs to be visualized. To address this challenge, this paper develops and compares different solution strategies for an interactive, persistent, and scriptable web-based visualization application.
These include different protocols for sending data points from the server to the client, such as HTTP, WebSocket, and WebTransport. The tests measure the transfer times of different dataset sizes and show that the WebSocket protocol outperforms the other two in this respect, while allowing a high degree of flexibility in software design due to its native duplex communication.

Furthermore, different techniques are tried to test and improve the processing in the backend as well as the rendering of the data points in the frontend. For the latter, different rendering techniques are tested, such as sending only the required data points, compressing them, and using SVG and HTML Canvas for rendering. To further improve the processing chain, a chunk-based approach is evaluated, which cuts the graph into smaller pieces that are processed individually and in parallel.

In addition, to enable persistence of the website, an architecture is designed to track the state of the website to maintain a history backlog, store the entire state, and restore it later. This is done using a combination of message-based communication and configuration in JSON format for each component’s state. These messages allow for traceable communication between components, while the JSON of each component can be used to revert to a potentially older state.

In addition, messages can be created directly on the website, either through a script or a web shell, so that the entire UI can be fully controlled and automated using the API.

Finally, the different solution strategies are combined into a demonstrator to show the capabilities of the found strategies in a real-world scenario.

Development of an XIDML File Concatenation Tool for Data Merging from Independent Sources

Rasit Uzun, Selma Aydin, Fatih Haciomeroglu, Furkan Aksoy, Mehmet Kekec and Ali Tahsin Kaymak – Turkish Aerospace*

Within the context of flight test instrumentation, while primary focus lies on equipping aircraft for data acquisition during evaluations, specialized tests often demand supplementary measurements independent of aircraft performance parameters. Illustrative examples encompass wind direction and speed crucial for specific flight regimes, and acoustic noise levels measured over instrumented areas during aircraft flyovers for external acoustic assessments. These ancillary data points necessitate independent acquisition utilizing systems separate from primary aircraft instrumentation (e.g., employing multiple KAM500 data acquisition systems). This document elucidates a methodology for consolidating data originating from at least two independent KAM500 systems into a unified dataset, effectively simulating a single source. In addition, software tool will be explained for XIDML merging and generating independent XIDML file.

AVALON. Automated Vibration Analysis and Localization Oscillation Nodes

Francisca Coll and Pedro Rubio – Airbus Defense & Space Spain

Real-time characterization of the aircraft flexible structure response plays a key role in various techniques such as Flutter testing, Load Alleviation, Vibration Suppression, etc. The current state of the art does not exploit all the possible benefits of having a “sensing” structure and AVALON is the right onboard automated tool to enhance the in-flight real-time characterization of a flexible structure, inferring relevant structural parameters as normal modes frequencies, structural damping, etc.

AVALON is a fully automated in-house tool based on jFlutter algorithms that is the official tool for flutter analysis in Airbus Defense and Space.

AVALON is funded by the Clean Aviation HERA (Hybrid Electrical Regional Architecture).

The initial objective of the development of AVALON is to be used in Wind Tunnel Tests on the HERA scale model, but there are multiple possible applications.

AVALON consists in two parts, one for automatic calculations and another, AVALONVIEW, for displaying results.

Both AVALON and AVALONVIEW can be used in online and offline mode.

The AVALON algorithm can be installed on a microcomputer, so it can be used on smalls UAVs like SIRTAP or EURODRONE.

This document will outline the technique used for the automatic modal parameter calculations, the architecture of the tool, different use cases and finally the different AITAVIEW interfaces.

Mitigating Costly T&E Using TRMC Solutions

Gene Hudgins and Juana Secondine -DOD OSD TRMC

The nature of telemetry often requires operators to be on location with receive system(s) or remote consoles, resulting in costly TDY and possibly a shortage of operators to support all scheduled events. To mitigate these issues, the US DOD’s Office of the Secretary of Defense (OSD) Test Resource Management Center (TRMC) has developed a remote-control capability (along with centralized data collection) to eliminate existing personnel requirements at both locations, greatly reducing operational costs and providing real-time insight to system status. The TRMC’s Joint Mission Environment Test Capability (JMETC) is a distributed LVC capability using a hybrid network solution for all classifications and cyber, and the Test and Training Enabling Architecture (TENA) is the middleware selected for use in JMETC Secret Network (JSN) events. TENA provides for real-time system interoperability, as well as interfacing existing range assets, C4ISR systems, and simulations – fostering reuse of range assets and future software systems. In addition, TRMC Enterprise Big Data Analytics (BDA) and Knowledge Management (KM) tools and techniques have the capacity to improve acquisition efficiency, keep up with the rapid pace of acquisition technological advancement, and to ensure effective weapon systems are delivered to warfighters at the speed of relevance, as well as enabling T&E analysts across the acquisition lifecycle to make better/faster decisions using data previously inaccessible or unusable. These capabilities allow the most efficient use of current and future TM range resources via range resource integration, critical to validate system performance in a highly cost-effective manner. This presentation will inform the audience as to the current impact of TRMC capabilities on the TM community; as well as their expected future benefits to the range community and warfighters.

Ease Datalake Fishing with Language Models

Vincent Malet and Adil Soubki – Airbus Operations

The Big Data Era laid the foundation for the current AI revolution by providing the massive datasets necessary to train advanced AI models. Now, AI, particularly Large Language Models (LLMs), promises to transform data analysis and utilization within organizations. However, a significant challenge lies in bridging the gap between these powerful models and the complex data landscapes inherited from the big data era. These « datalakes, » often characterized by diverse data types (structured, unstructured), heterogeneous access methods (REST APIs, SQL, PDFs, Spark), and a plethora of analytical tools (web UIs, dashboards, big data frameworks), present a significant barrier to efficient data exploration and analysis. While LLMs offer exciting new capabilities such as interactive natural language processing, agent-based workflows, and multi-modal data understanding, pre-trained general-purpose LLMs often lack the domain-specific knowledge required to effectively navigate these environments. Furthermore, fine-tuning these models can be prohibitively expensive.

This paper explores the implementation of EDIE, a chatbot designed to ease data access and analysis within legacy datalakes. We present strategies for integrating heterogeneous data sources from multiple systems into EDIE’s using an agent-based architecture. We investigate methods for selecting the optimal Language Model for this purpose, considering factors such as performance, cost, and domain suitability. Furthermore, we address the critical challenge of ensuring EDIE’s continued improvement and preventing performance regression by proposing a feedback-driven learning framework. This framework allows EDIE to learn from user interactions, adapting its behavior and knowledge to provide a more efficient and reliable data interaction experience within complex enterprise environments.

Overcoming Serial Processing Limitations in Flight Test Data Extraction

Mustafa Sinasi Pektas, Berkcan Kucukkasap, Ahmet Ata and Muhammed Peker -Turkish Aerospace

Flight test data is critical when a project is in the prototype stage, since it requires extensive analysis to determine the ideal system performance, stability, and operating features. Because of this relevance, it is common practice to deliver data to related engineering departments as quickly as possible by employing effective data extraction techniques, processing data faster, and communicating more effectively with system engineers. There are many tools available that handles the data processes and one of the well-known is the IADS. IADS is a compact and mostly error free program however its processing speed falls short for our needs and delays our data delivery time because of its serial data processing.

To overcome this issue, we developed a data extraction program using the “IADSDataInterfaces.dll” which is publicly available to all IADS customers. This dynamic library allows us to use the IADS generated file and alter the content of the flight test data as we like without needing to process the raw data acquired by the recorded systems. Using this DLL, we created a parallel processing functionality that uses multiple cores to further increase the speed and efficiency of the extraction process. In addition, we divided the input data into small parts to decrease the memory burden introduced when we implemented the parallel processing.

Our proposed solution aims for a user-friendly interface that is easy to define test points and process flight data from various test point simultaneously. The flight test schedule benefits from the parallel technique’s speed efficiency in data extraction and claims greater use of computer power.

This paper discusses the design, implementation, and performance benefits of our parallel processing solution. It details how the solution overcomes serial processing limitations, improves overall workflow, and integrates with existing systems. It also highlights the solution’s contribution to test and development processes and the time savings it provides on prototype projects.

TELEMETRY

Next-Generation Air-to-Air Networked Telemetry System for Extended Range Applications

Murat Imay, Serkan Sapaz and Hakan Özyürek – Tualcom / Deutsche Aircraft GmbH

This paper introduces a cutting-edge bidirectional telemetry system designed to revolutionize communication capabilities in flight test applications. The system supports downlink speeds of up to 8 Mbps and uplink speeds of up to 1 Mbps, with a range of up to 250 km. At its core, the system integrates TUALCOM data links with original waveforms, enabling a robust, multi-node mesh network. This innovative air-to-air network extends communication range by allowing airborne systems to act as nodes, forming a dynamic, masterless network that enhances distance to ground systems. The network features self-healing and self-forming ad hoc capabilities, along with precise RF distance calculation and time synchronization, providing critical time and location data during missions.

Unlike conventional telemetry systems, this solution delivers unparalleled flexibility and scalability, as the number of nodes in the network can be expanded as needed. The system’s physical layer capabilities enable long-range, high-data-rate communication, while the unique network layer algorithm ensures reliable relaying capabilities.

 This paper details the practical implementation of the telemetry system within the D328 Deutsche Aircraft flight test campaign, highlighting its advantages over traditional solutions. Key use cases include data acquisition and relay between multiple airborne systems and ground stations, demonstrating the system’s potential to significantly enhance range and reliability in demanding environments. By reducing dependency on direct line-of-sight, this approach paves the way for more robust and efficient telemetry operations in future aerospace applications.

Analyzing The Benefits And Costs For Chapter 7 Packet Telemetry

Benjamin Kupferschmidt and Kathy Rodittis – Curtiss Wright

The Inter-Range Instrumentation Group’s (IRIG) 106 Chapter 7 standard provides a method for embedding variable length, well-defined data formats within a Chapter 4 Pulse Code Modulation (PCM) stream. Chapter 7’s approach to embedding data streams within a PCM format offers several strengths and weaknesses. This paper will explore the pluses and minuses of the Chapter 7 standard and propose some alternative approaches that have been used successfully.

Challenges and Solutions in Bidirectional Telemetry Integration

Francisco Fernández Casuso – AIrbus Defence & Space

The purpose of this article is to show the evolution of the Airbus bidirectional telemetry project to achieve robust, efficient and high quality bidirectional telemetry. It will address the steps of the last stage, discuss the successes and the problems that have arisen from it.

The ultimate goal of this project is to develop two-way telemetry with equivalent capabilities in range, bandwidth and latency, while incorporating new features such as native networking or beyond line-of-sight communication (BLOS). To achieve this, a new system integrating high gain antennas with dipoles and advanced transmitter/receiver technologies such as beamforming and MIMO will be implemented.

The objective of this stage is to reduce and minimize the risks of bringing a new system to an aircraft that generates high costs, thus debugging the problems in a test environment easier to solve and with fewer risks. The aim is to achieve such confidence in the technology as to ensure that we can then go flying with the minimum probability of failure. Therefore, the aim is to confirm range, power and radiation data, but not only that, also to see how the communication works, what happens if there are link problems, etc.

This new technology implies a major change in aircraft and ground architecture, as well as a new way of working. Thus, this article will discuss the problems encountered and their mitigations. Finally, the next steps and future uses of the project will be discussed.

Detection of the Factors That Cause Telemetry Losses

Mahmut Kürşad Arpacıoğlu, Mustafa Melik Geçgel, İpek Çerşil Polat, Ayşe Bilsel, Hatice Çelik, Furkan Kamil Tut, Enes Alperen Şahin, Yeter Ateş, Muhammet Kürşat Serçeli, Arda Ulusan and Ökkeş Furkan Turna – Turkish Aerospace Industries, Inc.

Due to critical roles of the telemetry data in a flight test campaign it is aimed to transmit the data without loss however data losses occur for many reasons.

To determine the causes for the telemetry losses a study has been performed. The configuration of ground system components (antennas, receiver, BSS, etc.) in the telemetry system and the parameters obtained from those components recorded with the position and attitude information gathered from the aircraft under test has been monitored in real-time and analyzed in post process. The mentioned parameters which are analyzed made that possible to detect the reasons for the data loss and gave hints to improve the telemetry system components or the process of how the mission is performed.

This paper highlights the study which has increased the ability of tracking the a/c under test, gave indicators to detect if the malfunction has been occurred on a/c transmitting system or on ground receiving system, eased to detect the reason for the data loss such human / software error, physical obstacles between the transmitting and receiving systems or the shadowing effect of the a/c geometry due to the maneuver which has been performed.

Satellite Based Telemetry Transmission System

Blaise Barbe, Davy Ralliard Rousseau, Isabelle Carpentier and Louis-Marie Lecoeur -Safran Data Systems

SAFRAN DATA SYSTEMS is a leading telemetry and safety solutions provider with legacy customers such as Ariane and Vega and a growing customer base from New Space companies worldwide (America, Asia, Europe). To better prepare for the New Space era, a product line of satellite based telemetry solutions is developed to address all types of vehicles, trajectories, and spaceport requirements.

*PROPOSAL*

Traditional telemetry communication systems rely on ground stations located along the trajectory, which are costly to install and maintain, and constrain the possible trajectories.

For satellite based telemetry systems, the onboard unit takes its inputs from the vehicle, and transmits the telemetry information on a set of antennas. The transmission addresses communication satellites, but also ground stations if available.

These solutions are compatible with commercial communication satellites, in the L-band, but evolution to S-band and other frequency bands is already considered.

Special care has been taken to give full coverage for any space port on Earth (on the mainland and/or sea-based) and any trajectories, even polar based, with a comfortable link budget at all times, by selecting sufficient satellites.

At the same time, configuration has been kept as simple as possible to enable last-minute frequency changes or trajectory adjustments.

In fact, the communications systems does not require to know the actual trajectory ahead of time, and uses the position and attitude of the vehicle as inputs.

In preparation of the flight, the reservation of communication beams has also been optimized.
A specific mode for spaceport safety assessment will be included, so that the very same system can also be used for ground-based Flight Termination Systems which require continuous and low-latency telemetry reporting for the first minutes of flight, regardless of vehicle position and attitude.

A first demonstration flight is coming up in 2025, thanks to the partnership with VIASAT.

The ultimate solution will weigh less than 5kg, including antennas, excluding cabling.

*SYNTHESIS*

Safran Data Systems’ satellite based telemetry transmission system could prove to be the ideal solution for fast and easy recovery of flight data for the coming launch vehicles, for sizes ranging from nano to heavy.

*FURTHER EXTENSION*

Safran is also developing a prototype of uplink data transmission to the vehicle, this could be used for numerous applications, from inflight telemetry selection, return trajectory synchronisation, etc..

Architectural Design of an OFDM-Based Telemetry System

Xue Zhao, Xiaoqian Yi and Zitan Sun – Commercial Aircraft Corporation of China Ltd, COMAC

In recent years, the traditional PCM/FM telemetry system has increasingly struggled to meet the demands of flight test telemetry applications due to their low transmission rates and limited resilience against multipath interference and Doppler frequency shifts. To address these challenges, this paper proposes a novel telemetry system architecture based on Orthogonal Frequency Division Multiplexing (OFDM) technology. Firstly, the expected performance metrics of the proposed multi-carrier telemetry system are outlined, and link margin calculations are performed to verify its feasibility. Subsequently, the network architecture of the system is presented, followed by a detailed and efficient layered protocol stack design inspired by LTE and NR standards, to enhance system stability, efficiency, and manageability. Finally, the paper highlights the advantages of the proposed OFDM-based telemetry system, demonstrating its potential to overcome the limitations of traditional approaches.

Development of a first LEO / 5G UAV connectivity solution. Challenges and Opportunities

Jean Marc Gaubert, Adrien Pompée and Soundarya Srinidhi – Atmosphere

LEO / 5G could be a game-changer for flight test telemetry, offering high-speed, low-latency, and global connectivity at an affordable cost. Thanks to CNES and ESA support, ATMOSPHERE has pioneered this new field through the development of a first light LEO 5G connectivity solution. Compatible with Low Earth Orbit constellations and ground networks supporting 5G, as well as Iridium Certus satellite constellation, the solution developed by ATMOSPHERE was certified in 2024. The airborne terminal developed by ATMOSPHERE is a low-swap unit, primarily targeting unmanned aircraft vehicles (UAV) and stratospheric balloons. ATMOSPHERE currently collaborates with several OEMs, integrators and agencies on pilot operations. Initial tests have successfully demonstrated the capability to transmit platform telemetry and video stream in real-time over satellite and terrestrial networks. The proposed paper will present the challenges faced by ATMOSPHERE in the development process, provide preliminary return of experience from pilot operations, and introduce future opportunities for flight test telemetry use cases.

Implementation and Field Demonstration of a Spectrum Management, Risk Mitigation, and RF Control System

Joseph Molnar, Lam Pham, Matthew Dillon, Er-Hsien Fu, Lan Tran, Matthew Feid and Eric Makara – US Naval Research Laboratory

The radio frequency (RF) spectrum is a vital resource that has become increasingly limited due to rising demand and inefficient spectrum allocation and assignments. With spectrum availability shrinking, modern spectrum-dependent systems (SDS) must coexist within co-assigned bands. Additionally, efficient spectrum management requires real-time monitoring to identify potential assignment errors and unauthorized access in the band. At the Naval Research Laboratory, we managed, provided technical oversight, and tested the development of a spectrum management system consisting of three core components: RISA (Risk Informed Spectrum Access), OSCAR (Operational Spectrum Comprehension, Analytics, and Response), and MICCA (Multi-band Control Channel Architecture). We worked with our industry partners to develop the three components. These partners included: Peraton Labs (OSCAR), Leidos (RISA), and Shared Spectrum Company (MICCA). The objective of RISA is to provide risk assessment of planned and ongoing field events through multi-swarm particle swarm optimization (MS-PSO) and deep learning of the signals environment to identify authorized occupants. OSCAR serves as an intuitive visualization tool that reduces the cognitive load for spectrum managers through identifying, localizing, and summarizing assignment violations. MICCA provides an approach for reliable delivery of spectrum plans/policies that was issued by the spectrum manager via OSCAR to the SDS systems. MICCA also monitors the position and performance at each SDS in order to provide the diagnostics to OSCAR and RISA. A Capstone field demonstration event in August 2024 was conducted to evaluate the implementation of the integrated system. The effectiveness of the system’s capabilities was evaluated through a set of scenarios. The scenarios were designed to demonstrate multiple functions: the evaluation of spectrum risk throughout an evolving exercise, the identification and localization of entities violating spectrum assignments, the spectrum policy dissemination, monitoring and control of spectrum dependent systems, and the identification and characterization of spectrum occupants. This paper presents the system-of-systems, describes the evaluation scenarios, presents the results, and provides analysis and observations for enhancement.

LDPC Forward Error Correction for Telemetry System of Civil Aircraft Flight Test

Yi Zhou, Xiaoqian Yi and Zitan Sun – COMAC Flight Test Center

In the flight testing of civil aircraft, telemetry signals are influenced by various factors such as noise, reflection, occlusion, and atmospheric absorption. These factors can increase the Bit Error Rate (BER) of the telemetry signal received through the telemetry link, ultimately leading to a degradation in signal quality. This paper discusses Low Density Parity Check (LDPC) forward error correction, which can be integrated into the telemetry link to enhance link margin and rectify random errors arising from transmission anomalies. An LDPC encoder and decoder module were incorporated to establish a new telemetry link utilizing SOQPSK modulation. Experimental results demonstrate that LDPC is an effective error correction method; furthermore, the IRIG 106 recommends its use for telemetry link.

Telemetry Spectrum Encroachment Post WRC-23

Tim Chalfant and Sergio Penna – ICTS

A review of international and domestic spectrum issues that can challenge the future use of radio frequency telemetry after the recent 2023 World Radiocommunications Conference. Several agenda items addressed there have a potential for telemetry spectrum encroachment and are presented in this paper. Topics of interested in future World Radiocommunications Conferences are also presented. International telemetry vendors, suppliers, and users need to be aware of, and potentially engage with their national administrations on these items.

The authors represent the International Consortium for Telemetry Spectrum (ICTS, www.telemetryspectrum.org) which was formed in 1999 and is chartered under the sponsorship of the International Foundation for Telemetering (IFT). The IFT (www.telemetry.org) is a non-profit organization dedicated to serving the professional and technical interests of the telemetering community.