IMA (Integrated Modular Avionics) for Small Air Transport

Project Information

IMASAT

Grant agreement ID: 785523

DOI

10.3030/785523

Project closed

EC signature date 7 February 2018

Start date 1 March 2018

End date 30 June 2022

Funded under

• SOCIETAL CHALLENGES - Smart, Green And Integrated Transport

Total cost

€ 1 246 716,25

EU contribution

€ 869 550,00

Coordinated by

AERTEC SOLUTIONS SL
Spain

Periodic Reporting for period 3 - IMASAT (IMA (Integrated Modular Avionics) for Small Air Transport)

Reporting period: 2021-03-01 to 2022-06-30

Summary of the context and overall objectives of the project

Description of project context and objectives.

The consortium between AERTEC and CLUE is developing IMASAT “Integrated Modular Avionics for Small Air Transport”. IMASAT is focused on the design, manufacturing and qualification of a new Computing Node suitable to be used as Flight Control Computer for small air transport (SAT).
The IMASAT project attends to Clean Sky aim to revitalize the European SAT industry by encouraging the insertion of a range of new and cost effective technologies in the area of systems for a future new generation small transport aircraft (Airframe ITD WP B3.5 and Systems ITD – WP S.3). The aim of the research project is to define and implement IMA concept for SAT, so that European industry players will be able to adopt fly-by-wire (FBW) systems to reduce the weight of avionic systems, reduce maintenance operations and enhance safety by improving the human-machine interface and automatically help stabilize the aircraft.

(Figure 1 - Overview of IMASAT architecture)

IMASAT system is based on a small, stackable, custom form-factor integrated modular avionics (IMA) computer designed to present reduced weight, volume, and power dissipation. Each IMASAT unit could represent a Processing Node connected to a safety-critical Ethernet network and physically segregated from other resources such as Remote Data Concentrators (RDC), Remote Electronic Units (REU) or Remote Power Controllers (RPC). A main network high-speed AFDX safety Ethernet-based fulfilling ARINC 664 requirements will meet the requirements of low costs and data integrity in flight safety critical systems.

(Figure 2 - IMASAT chassis)

IMASAT Node's software architecture is determined by the operating system, PikeOS, that creates and manages different partitions. These partitions are isolated from each other, which means that a problem in a partition cannot affect the correct behaviour of the software running in the other partitions. In PikeOS 5.1 Hypervisor is DO178 DAL-A certified.
A test bench developed for IMASAT provides comprehensive testing without using an assembled final product. It is dedicated to define, run, control and monitor the different simulations to be executed in IMASAT unit to test its capabilities. (hardware-in-the-loop, HIL, test). By allowing the system under test to interact with a simulated use case, it is possible to test early and often to uncover as many software defects as possible.n.

(Figure 3 - IMASAT test bench)

Work performed from the beginning of the project to the end of the period covered by the report and main results achieved so far

Description of the work during First period

Since the beginning of the project, the consortium has defined and described the specifications and ensured his compliance along the design phase. From these requirements, collected in the System Requirements Report, the designers and specialists started to work on the technical solution. They designed and detailed a product in three phases: a high-level overview of IMASAT system main hardware and software parts, conceptual design, and a preliminary design with a deeper insight in the system and the final design of the system that meets customer requirements as well as standards and regulatory requirements.
(Figure 4 - HW-SW levels)
In this sense, a full analysis of the system has been performed to prove that system requirements have completely and correctly been understood and that all technical requirements are implemented. Simulations thermal and vibrations have been carried out and a safety analysis has been performed to prove the reliability of an IMASAT node.
(Figure 5 - Thermal simulation results)
Concerning the test bench, its technical, performance, operational and support characteristics and the external communication interfaces have been defined in order to be able to debug the hardware and software assumptions
(Figure 6 - IMASAT Test Bench - Architecture Overview)

During the 2nd reporting period.

it has been reached to an agreement on the environmental tests to be performed, by prioritizing TM (Topic Manager) and CLUE needs, confirming the tests’ categories, considering the necessary auxiliary equipment, and scheduling the laboratory tests. Three companies were requested for quotation and schedule estimation on the agreed environmental tests.
it has been attained an agreement on the form and contents on PikeOS training provided by SYSGO.
IMASAT Computing Node prototype and its Test Bench have been developed/manufactured (Figure 7 and Figure 8). Three versions of the Computing Node have been developed (v1, v2, new version).
the Built-in-Test (BIT) of IMASAT prototype has been defined, including; (PBIT), (CBIT), (IBIT) and HMR.
a NXP T2080 dev kit was delivered to TM, along with the necessary support to configure PikeOS on it.
the acceptance tests procedures of the Computing Node have been defined.

During the 3rd reporting period.

SW and FW developments have been made to cover all the agreed interfaces:RS, ETH, GPIO, CAMBUS , Analog Input, Analog Output, and AFDX .
Improvement of the performance of the equipment, especially in relation to processing speed.
Environmental tests according DO-160 were successfully carried out
An automated testing system was implemented, which greatly reduced the time required for the execution of tests.
Finally, all the defined tests were successfully completed and an updated computer node unit was delivered to the TM.


The main Dissemination channel of the project has been the project website www.imasat.eu.
The consortium also has disseminated project results through their attendance and participation in international conferences and trade fairs, such as OPTRO in Paris, TRANSFIERE in Malaga and ILA in Berlin.

Progress beyond the state of the art and expected potential impact (including the socio-economic impact and the wider societal implications of the project so far)

IMASAT pursues the definition of an IMA architecture and the basic building blocks of a highly scalable system for safety critical applications with the aim of supporting a fly-by-wire system.
IMASAT project will contribute to the safety and efficiency of small aircraft operation by enabling the implementation of fly-by-wire systems, towards a More Electric Aircraft, thus further benefiting from the use of such technology increasing flight and operation efficiency and lowering environmental impact through:
• lower cost, when compared to current nodes, it will reduce the cost approximately by a third.
• lower maintenance costs, when compared to mechanical controls, along with a better fault isolation and test.
• the increase of the flight stability (safety) derived from the application electronically computed control laws as part of the fly-by-wire system.
• a save in fuel through the reduction of the weight, size and energy of power systems (electric vs. hydraulic) and actuators (EHA, EMA vs. SHA) required to actuate flight controls.

IMASAT will contribute to the revitalization of the European small aircraft industry by generating and delivering high added value knowledge in cutting-edge technology fields, namely avionics, historically dominated by American companies.
IMASAT impact into society can be measured in terms of number of employments generated by increasing the competitiveness of the Andalusian regions. In fact, this project would impact to empower a group of companies that are developing aerospace systems in the PTA (Technological Park of Andalusia): AERTEC and CLUE as SME, in collaboration with other local suppliers. In addition IMASAT is 100% aligned with the RIS3 Area “Advanced Transport Systems in the aeronautics, aerospace and naval industries”, part of Andalusia’s Smart Specialization Strategies

Figure 8 - TB With LRU

Figure 2 - IMASAT chassis

Figure 5 - Thermal simulation results

Figure 1 - Overview

Figure 6 - TB - Architecture

Figure 7 - LRU

Figure 4 - HW-SW levels

Figure 3 - IMASAT test bench