AI4AIT

Artificial Intelligence For Augmented Reality In Satcom Assembly, Integration And Test (ARTES AT 4A.084)

STATUS | Completed
STATUS DATE | 28/01/2025
ACTIVITY CODE | 4A.084

Objectives

The project objectives are to enhance autonomy in decision-making for quality assurance during spacecraft Assembly, Integration, and Testing (AIT). The project focuses on developing an innovative system that integrates augmented reality (AR) and artificial intelligence (AI). By using sensor data from AR devices and AI-based image recognition, the goal is to compare spacecraft CAD models, pictures and videos with the physical assembly and provide the operator with cues to ensure efficiency, precision and accuracy. A collaboration with AI, AR and AIT experts and the use of representative facilities ensures the solution aligns with real-world operational needs. 

Challenges

The project faced some challenges worth noting. OCR struggles with complex backgrounds, and arbitrary alphanumeric sequences. Object Detection’s reliance on real-world data limits flexibility when only CAD models are available. Similarly, 6D Pose Estimation lacks the precision required for certain high-accuracy tasks. Real-time AI processing introduced further issues, including reduced HoloLens application framerate, stream delays causing lag in AI responses, and degraded performance in features like voice dictation.

Additionally, video streaming impacted reliability for external sharing.

System Architecture

The AI4AR system architecture combines a computer and an AR headset to support augmented reality in complex assembly tasks like
satellite integration. 

The computer manages core computational tasks, with the following modules: Detection Module (Identifies and locates objects in the
assembly environment using advanced algorithms); 6D Pose Estimation Module (Ensures precise object and headset positioning for accurate virtual overlays); OCR Module (Extracts text from labels or instruments for validation and contextual guidance); and Communication Module (Enables fast, low-latency data exchange with the AR headset).

The AR headset acts as the operator’s interface, providing augmented visualizations and guidance, capturing real-time visual and depth data for detection and pose estimation; aligning virtual overlays with the user’s perspective and also synchronizing data with the computer for real-time feedback.

Plan

 The project was initially planned to have a full duration of 24 months.

The following different work packages were pursued: WP1 Preliminary Design, which included the “Output 0 (Defined System Scenario)
Review” and the “Output 1 (Finalised Technical Specification) Review”;

WP2 Detailed Design, which included the “Output 2 (Selected Technical Baseline) Review” , the “Output 3 (Verified Detailed Design) Review” and “Output 4 (Implementation and Verification Plan) Review”; WP3 Implementation, which included the Applications Review; and WP4 Validation and Way-Forward, which included the “Output 5 (Verified Deliverable Items and Compliance Statement) Review” and the “Output 6 (Technology Assessment and Development Plan) Review”. 

Current Status

Project completed, all goals achieved.

EREBUS

- European Reprogrammable Battery Unplugging System

STATUS | Completed
STATUS DATE | 28/01/2025
ACTIVITY CODE | 4F.137

Objectives

The focus of our project was to research, develop, and test a passivation method specifically tailored for Li-ion battery cells to be integrated into small satellites and CubeSats. Our aim was to ensure compliance with the Space Debris Mitigation requirement for passivation, as outlined in the ECSS-U-AS-10C Rev.1 [2] and ISO 24113 6.2.2.3 [3] standards, without introducing any additional risk during normal satellite operations. It was essential for the passivation device to be compatible with commercially available cells commonly used in this type of mission and for satellites operating in both Low Earth Orbit (LEO) and Geostationary Orbit (GEO) applications. 

The project was initiated with the primary objective of addressing the critical issue of space debris and facilitating the implementation of international regulations pertaining to this matter. To validate the efficacy of the proposed approach, realistic degraded battery cells were manufactured and successfully integrated with the prototype electronics. Through extensive testing and refinement, the device has now reached a stage where it is ready to be produced as a proto-flight model for a real demonstration mission.

Challenges

Our research contributes to the broader effort of mitigating the risks associated with space debris. Furthermore, the successful development and implementation of an effective passivation method for Li-ion batteries in small satellites will enhance the overall safety and sustainability of satellite operations in the ever-expanding space environment.

System Architecture

The device has been designed to seamlessly integrate into next-generation small satellites, prioritizing factors such as its compact form factor (PC/104), which ensures compatibility with most CubeSats, its lightweight construction, and its versatile electrical interface.
The incorporation of a reprogrammable microcontroller enables active control over all components of the board, facilitating the establishment of secure and well-defined initial conditions. This feature not only mitigates the risk of accidental satellite activation during ground operations or after the EOL phase but also allows for the reprogramming of the cut-off voltage to accommodate different types of battery cells. Several components, including microcontrollers, have been carefully selected for their radiation hardness to ensure high reliability in operation. The system has undergone extensive validation to ensure its capability to handle loads of up to 155 W (34 V or 8 A), guaranteeing the safe and efficient management of power requirements. Furthermore, the device employs an RS422 interface.

Five candidate cells were initially identified. Key evaluation criteria included energy density, capacity, cycling performance, operating temperature range, safety features, and cost. Based on this assessment, two cell types were ultimately chosen: “Cell A,” a power cell representing LEO missions, and “Cell B,” an energy cell representing MEO and GEO requirements.

Plan

Contract MLS list:

Progress (MS 1) – achieved

Progress (MS2) – achieved

Finale Settlement (MS3) – achieved

Current Status

The project passed the Final Review and it’s officially closed.

LEO FLOPs

OPTICAL FEEDER LINK SITE-DIVERSITY PROTOCOLS FOR SATELLITE CONSTELLATION NETWORKS

STATUS | Ongoing
STATUS DATE | 17/01/2025
ACTIVITY CODE | 3A.170
LEO FLOPs

Objectives

The design and demonstration of link protection and restoration protocols, suitable for enhancing the reliability of optical feeder link systems. The solution shall be commercially competitive compared to radio frequency (RF) feeder systems for low Earth orbit satellite constellations, and result in similar or better performance with respect to key system parameters like latency, jitter or throughput.

Challenges

Reliable connectivity to a LEO constellation using optical feeders faces major challenges: 

  • Short contact times require a large, spatially dispersed network to ensure availability.
  • Cloud cover and atmospheric turbulence induced outages decrease the planning reliability of these links. 
  • The solution needs to commercially competitive at very high data rates (>=100Gbit/s), otherwise RF solutions prevail.

System Architecture

The system architecture will become available after the conclusion of system trades.

Plan

The project is split into two stages:

  • Analysis and evaluation of existing methods, along with the assessment of feasibility for implementation into the emulator.
  • Implementation, performance benchmarking, and result analysis.

Current Status

The project has started and completed reviewing literature and assessing state-of-the-art.

ARTES AT Kr

- Electric Propulsion Technologies Operating on Krypton Propellant

STATUS | Ongoing
STATUS DATE | 15/01/2025
ACTIVITY CODE | 4B.129
ARTES AT Kr

Objectives

The objective of the project is to mature the cathode of the PPS® low power thruster, namely the PPS®X00, for an optimized operation with Krypton as propellant, in view to offer a competitive efficient propulsion solution meeting the small satellite market demand, and of particular interest in the mega-constellation segment where the xenon availability is a key issue.

The following tasks are covered by the project activities: 

  • First, the design and manufacture of a highly flexible device functionally and thermally representative of a hollow cathode, so-called BTC. 

  • Then functional and thermal characterizations carried out with this hardware by varying the dimensions of the functional parts of the emitter’s housing, the material of the emissive element, and the propellant gases.

  • The third step consists in refining the cathode model developed by Safran by adjusting the modelling parameters after the measurements performed on the BTC

  • Finally, the design, manufacture and test a BBM “krypton hollow cathode” based on these results and complying with the specification.

  • The activities and logic defined at the beginning of the project benefit from synergies with the ARTES C&G PPS®X00 project.

Challenges

The world of space is constantly evolving. Depending on the health, economic and geopolitical context, the space market ecosystem is considerably affected and has to reinvent itself regularly. The compatibility of the propulsion system’s operation with an available propellant gas, krypton, is an asset enabling us to offer an effective, low-cost solution for a low-power Hall-effect thruster, within a very tight time-to-market.

System Architecture

A Hall thruster is composed of an anode assembly and a cathode assembly. To create the thrust a magnetic field is generated in a dielectric chamber to achieve the Hall effect required to ionise the gas, confine the plasma and accelerate the ions under an electrical potential. Electrons are supplied to the anode block by the external cathode to initiate and maintain the discharge. These assemblies consist mainly of an anode/gas distributor, a discharge chamber, a magnetic system, a hollow cathode, gas and power supply lines and mechanical interfaces.

The basis of the project is to generate an optimal design in terms of cost and performance.

The PPS®X00 cathode architecture and assembly processes simplifications compared to legacy designs enable to reduce drastically the manufacturing cycle.

Plan

The major phases of the project are:

  1. Design and manufacture a highly flexible device functionally and thermally representative of a hollow cathode. 

  2. Perform functional and thermal characterizations of this device by varying: i/ the dimensions of the functional parts, ii/ the material of the emissive element, iii/ the propellant gases.

  3. Refine the cathode model developed by Safran by adjusting the modelling parameters after the measurements performed on the device

  4. Design, manufacture and test a BBM “krypton hollow cathode” based on these results and complying with the specification

Current Status

All the elements to pronounce a TRL6 maturity of the PPS®X00 cathode operating with krypton are available: necessary justifications, mitigation of risks associated with critical technologies, compliance with technical and commercial requirements, and industrial conditions such as the whole manufacturing chain consolidation.

The future development phase mainly consists in the assessment of the residual risks to consolidate the flight target definition through lifetime tests with Krypton, additional analyses and tests at component level. These activities are necessary inputs for the qualification phase, and entry into service in 2025.

Compact 8kV Class High Voltage Planar Transformer for Electronic Power Conditioning Units

- Compact 8kV Class High Voltage Planar Transformer for Electronic Power Conditioning Units

STATUS | Completed
STATUS DATE | 22/12/2024
ACTIVITY CODE | 5C.382
Compact 8kV Class High Voltage Planar Transformer for Electronic Power Conditioning Units

Objectives

The objective of this activity is to design and develop a high voltage power transformer in planar technology for Electronic Power Conditioning Units (EPC) used to drive travelling wave tubes.

The aim is to develop a novel transformer design solution not existing today in Europe for up to 8kV class of EPCs (with research of margin up to 10kV). 

A transformer engineering model is designed, manufactured and tested in a  representative environment to validate the developed concept for space application.

The main intermediate objectives of this project are: 

  • To establish a detailed requirement specification for the high voltage planar transformer,

  • To define a program (in Excel), based on the build-up in order to compute the tracks size of primary and secondary windings, the leakage inductance, the copper losses of the secondary and primary windings, the core losses, the resonant push-pull losses and rectifier losses,

  • To define thermal and electrical models of the High Voltage Planar technology,

  • To review and de-risk the available technologies and processes available in accordance with the technical requirements defined,

  • To minimise the manufacturing complexity and to ease flexibility during production aiming at a short time to delivery.

Challenges

The main technological challenges are the management of the high electrical fields inside the planar transformer assembly, and the thermal management of the transformer.

The chosen design needs to manage high voltage design rules in PCBs, while at the same time using a more complex build-up than high voltage PCBs currently used.

Thermal design needs to be optimized by using innovating solutions such as optimizing the transformer build-up and improving thermal interfaces with the structure.

System Architecture

Resonant transformer topology working at high frequency.

The Planar transformer technology is based on a high voltage multilayer PCB equipped with its ferrites, thermal conductive material and mechanical fixations.

The secondary side is a single or multiple windings and the primary side is a push-pull type so double windings with a common point.

Plan

The project’s work plan is based on the following methodology:

  1. Based on the state of the art of the Travelling Wave Tube Amplifier, to build the definition of a detailed technical requirement specifications for planar transformer,

  2. To study suitable technologies to achieve a high voltage transformer in planar technology based on a technical trade-off and specific de-risking evaluation activities as High Voltage withstanding aspect,

  3. To study and optimize the electrical and thermal concept of such technological assembly. This step includes detailed calculation and optimization of magnetics tools (including software calculation tools),

  4. After the manufacturing of an Engineering Model (Elegant Bread Board – EBB), to test the High Voltage Planar technology in a realistic EPC environment. The tests sequence includes a Thermal Vacuum test sequence covering GEO mission needs.

Current Status

The main achievements are: 

In the frame of the project Requirements Review (RR):

  • The feasibility study to address the technology to the following TWT tubes has been validated: 150W Ku, 40W Q, 250W Ka, 170W Ka, 300W Ku, 150W C, 75W C, Dual 70W Ka and Compact Dual Ka/Ku TWT’s (80W RF) and for multi-tube constellations market, 

  • The confirmation of implementation feasibility has also been successfully performed ; this study included the following tasks: definition of the preliminary mechanical architecture of the technical solution, planar losses optimization, PCB build-up, preliminary thermal analysis and preliminary electrical fields analysis.

In the frame of the project Technical Design Review (TDR):

  • Several electrical optimizations have been performed including parasitic capacitors computations and leakage inductance distribution,

  • Based on these optimizations, the development of the Planar/PCB build-up has been pushed including thermal and Electrical field analysis,

  • The derisking of the PCB technologies including incoming tests definition, High Voltage ageing behavior (with the definition of a specially dedicated representative test vehicle) and materials performances such as outgassing tests and dielectric strength.

In the frame of the project Preliminary Design Review (PDR): 

  • The definition of the Elegant Breadboard (EBB) ; designed taking into account the challenge to establish a compromise between high voltage insulation properties and sufficient thermal drain capabilities of the HV planar transformer technology studied in the frame of this project.  The demonstrator definition was based on Quadral EPC adapted to the selected TWT’s, i.e. 170W Ka. Detailed calculation and optimization methods for magnetic, electrical and thermal designs have been performed. The design took into account manufacturing and assembly properties in order to minimize the manufacturing complexity and to ease flexibility during production aiming at a short time to delivery. 

In the frame of the project Final Review (FR) : 

  • The planar transformer technology has been exposed to space representative environment. After a first step covering the ground test sequence, a TVAC sequence of 130 thermal cycles has been successfully performed in order to verify the high voltage design and environment effect (including the effect of the local increase of pressure). 10 cold starts at -40°C have also been performed. The test has then been pursued with success with a HV life test at +70°C base plate in order to reach a total test duration of 1500 hours. The test sequence also included thermal characterization under vacuum in order to validate the thermal model related to the evaluated technology.

MMC

- Qualification of MMC Cathodes

STATUS | Ongoing
STATUS DATE | 21/12/2024
ACTIVITY CODE | 5C.321
MMC

Objectives

The achievement of high output power requires a higher energetic electron beam. Technological bricks are more and more challenging, developments for components and materials are getting marginal.

In order to achieve a high electronic flow, with reduced geometrical dimensions, an advanced new electron emission device (MMC) is needed, for a constant high beam current density. This MMC device shall be capable for 5 A/cm² electronic flow through the TWT interaction range. Obviously, the electron ejection has to function constantly for more than the 15 years of the cosmic mission life.

MMC objectives

The MMC emitter is developed from actual MM-type technology, at THALES as a new high current density electronic source. It allows an increase of the current density by lowering the extraction energy for electronic emission.

The new MMC emitter-design is already in use in telecommunication tubes on ground, for high power TWT’s. The non-terrestrial qualification includes a complete batch of MMC-devices, further specific test vehicles and qualification tubes in order to verify the performance of the MMC devices either by accelerated or standard life testing.

Based on a successful qualification, the MMC emitters will serve THALES’ actual and new development projects, where the high emission current density is mandatory.

Challenges

The development of the MMC emitter for 5 A/cm² with 15 years life time can be considered as an evolution out of the well approved and reliable MM-type technology. By lowering the extraction energy for electronic emission, the MM-technology could be systematically improved and verified. Consequently, the MMC device for non-terrestrial application represents the follow-on for the MM-type emitter, including a general process update, while maintaining the reliability aspects of the actual MM–type emitter. In detail, prior to the qualification of the MMC-emitters a further optimisation step for increasing performance and reliability is done by adjusting the manufacturing processes.

System Architecture

The electron beam is generated by the MMC emitting device. By increasing the current density the electron beam becomes more powerful and a higher output power of the TWT can be reached.

High power TWTs are designed such, that they can handle maximum microwave energy, which is automatically correlated to the tube efficiency. So, – under the consideration of a sufficient margin – the following main parameters are adjusted to their physical / material optima: 

  • Temperature

  • Thermo-mechanical stress

  • Thermal gradients

  • Thermal conductivity

  • Electrical field strength

  • Long-term stability

The MMC electron source has to fulfil all of the above criteria, which sometimes need to choose a compromise on materials and processes. Therefore, the selected materials and processes play an outstanding role in this assembly and need to be chosen very carefully.

Plan

The project is divided into three blocks, each finalized by a dedicated milestone.

The first is focused on the process engineering updated and closed by the Preliminary Design Review (PDR/TRR). 

Followed by qualification tests on subassembly level and specific test vehicles, which were finalized by the Critical Design Review (CDR).  Finally, the qualification test on tube level for a 170W Ku-band TWT THL12170C+ was successfully performed and evaluated for the final review.

Current Status

The qualification campaign of the MMC cathode was successfully performed with real improvements for THALES and their customers. With a significant increase of the permissible emission current density up to 5A/cm² future gun designs can be improved with reduced beam compression and therefore improved beam focusing. The customer can expect improved live time behaviour, due to the fact that a chromium-doped MM cathode will ensure improved barium coverage over a long life time. The cathode size can be potentially reduced due to increased current density or kept constant to replace MM cathodes with improved life time behaviour.

MESNET

- Mesh and Associated Carrying Net for Deployable Reflector

STATUS | Ongoing
STATUS DATE | 21/12/2024
ACTIVITY CODE | 5B.138

Objectives

The objective is to increase significantly the TRL of a European Metallic Mesh (including network below) for large deployable antenna applications up to Ku-band. Two types of knitting patterns are investigated in terms of RF-performance (reflectivity and PIM), mechanical characteristics and manufacturing processes. A five-meter demonstrator mesh and network has been manufactured and tested.

MESNET objectives

 

Challenges

The assembly of a five-meter diameter network structure with mesh. The access ability is challenging because you need to have access to the middle during the assembly which is only possible from one side or via a jigs crane and/or stages.

System Architecture

The carrying net is made of single unidirectional Quartzel rovings between two Polyimide tapes. The carrying net creates faceting triangles. The crossing points are assembled by pins that are inserted into punched holes of the rovings. Within these connecting pins, the tie cables are installed. These consist of an Aramid thread and a spring that tension the upper and lower carrying net to their paraboloid shapes.

The RF-reflective surface of the reflector is made of a mesh manufactured out of gold-plated tungsten.

Plan

The project had a standard approach, design, sample campaign. Based on the result of the sample campaign the demonstrator manufacturing and assembly have been performed. 

Current Status

The required TRL 5 has been fulfilled for the mesh (even TRL 7), the carrying net (even TRL 6), and the tie cables. Based on the performance data gathered from the project activity, several lessons learned have been identified allowing HPS to make further improvements to the design in future follow-up projects.

The ring structure used in MESNET was a rigid assembly which functioned as support jig. The next step to a potential following up project is the combination with a foldable lightweight structure to have a full large deplorable reflector for a potential EQM.
 

KaUF EQM

Ka-Band User Feed Chain EQM

STATUS | Ongoing
STATUS DATE | 20/11/2024
ACTIVITY CODE | 5B.197
KaUF EQM

Objectives

Picture: KaUF EQM (Photo: Airbus)
Picture: KaUF EQM (Photo: Airbus)

Starting point for this activity was the EM design of a combined Tx-Rx Ka band feed chain for user application, developed in a previous program.

This feed chain was further developed and qualified as EQM in a scalable feed cluster. Therefore, beside the RF performance, mass and dimensions were important design drivers. The feed cluster in this program consists of a waveguide panel, designed as beam forming network, carrying 16 horn-polariser assemblies.

Challenges

The design of the Ka band feed chain needs to allow the application in a scalable feed cluster to be used as feed for a multi spot beam antenna. To be able to achieve narrow beam spacing and a compact feed size, the outer diameter of the feed chain was chosen to be 30mm. To achieve a good RF performance with such accommodation constraint, while fulfilling the environmental requirements was the main challenge of this program.

Plan

The project started with the mechanical analysis of the EM feed chain model of the previous program. Design iterations to balance RF performance and mechanical properties followed.

In parallel a waveguide panel with an integrated distribution network was designed. Both designs were performed under the constraint of scalability with respect to the number of feeds in the cluster.

After the detailed design phase all components were manufactured, integrated and tested according to the requirements.

Current Status

The project is completed successfully. 

Additively Manufacturing technology 3D-printed K/Ka Antenna-Feed System with integrated RF, Thermal and Mechanical Functionalities

Additively Manufacturing technology 3D-printed K/Ka Antenna-Feed System with integrated RF, Thermal and Mechanical Functionalities

STATUS | Ongoing
STATUS DATE | 20/11/2024
ACTIVITY CODE | 5B.182 P2
Additively Manufacturing technology 3D-printed K/Ka Antenna-Feed System with integrated RF, Thermal and Mechanical Functionalities

Objectives

Describe in less than 200 words the objectives of the project. 

The satellite communication market is evolving towards medium-volume production of antennas and associated front-ends. Indeed, in GEO applications, complex focal plane arrays of hundreds of antenna-feed chains and BFNs are required to implement Tbps VHTS systems. In LEO and MEO applications, constellations of several hundreds or even thousands of low-cost small satellites are already in operation or will be deployed soon. 

In this framework, additive manufacturing (AM) technologies are being steadily investigated and exploited for the development of RF equipment for satellite communication payloads. Indeed, AM technologies provide several advantages with respect to conventional machining, among which are free-form capability and fit-for-purpose design. These two specific aspects of AM enable the integration of different functionalities in a single monolithic part, thus reducing the number of parts, costs, lead time, and MAIT activities. 

The present project aims at developing through AM a monolithic K/Ka-band dual-circular-polarization antenna-feed system with integrated RF, thermal and mechanical functionalities, intended for GEO High Throughput Satellites.

Challenges

Additive manufacturing technologies offer several advantages in the development of highly integrated RF systems with additional functionalities. However, they also present critical aspects in terms of dimensional accuracy and surface roughness, when RF equipment working at K/Ka bands and in dual-circular polarization are targeted. In this view, one of the main challenges of the present project deal with the RF, mechanical and thermal co-design of the antenna-feed system capable of minimizing the impact of the manufacturing process on the performance. In parallel, challenges apply also on the manufacturing process in order to optimize the production parameters for the intended application.

System Architecture

The K/Ka-band dual-circular-polarization antenna-feed chain developed in the present project consists of a smooth-wall feed-horn and an asymmetrical feeding-network. 

Since a dense focal plane array is considered, the relevant feeding network has to fit within the radiating aperture of the feed horn. Moreover, it was considered the additional goal to minimize the transversal dimension of the feeding network to make feasible its potential application to arrays with smaller lattice steps. Indeed, asymmetric configurations lead to very streamlined geometries, compatible with lattice steps of the focal-plane array in the order of 20 mm, although at some expense in terms of performance (primarily, port-to-port isolation in polarization and XPD). To understand the applicability of these configurations, three different architectures were investigated.

The mechanical design of the EM integrates the adapters towards the standard measurement setup. The design of the thermal circuit integrated in the feeding network was carried out by considering a requirement of thermal dissipation equal to 2.5 W. After a trade-off study and considering the minimum tube dimensions, a Mechanically Pumped Fluid Loop (MPFL) system was selected.

Plan

The project plan consists of one phase, including the following milestones:

  • Requirements Review (RR), focused on requirements at system, antenna and antenna-feed chain level, regarding RF, thermal and mechanical aspects.

  • Mid-Term Review (MTR), focused on the preliminary RF design of the antenna-feed system and bread-boarding of key building blocks.

  • Critical Design Review (CDR), aimed at the consolidation of the RF, thermal and mechanical co-design and additive manufacturing route of the EM.

  • Test Readiness Review (TRR), focused on manufactured EM, test plan, and measurement setups and procedure.

  • Test Review Board (TRB), aimed at the discussion on the comparison among predicted and measured performance of the EM, including RF, thermal and mechanical responses/properties.

  • Final Review (FR), including all the activities carried out during the project and discussion on lessons learnt and follow-on activities.

Current Status

The project was successfully completed. Indeed, the tests performed on the EM confirm the validity of the RF, thermal and mechanical co-design and manufacturing approach and pave the way for a continuation of activities aimed at obtaining a higher TRL.

DC3

Digitally Controlled DC/DC Converter

STATUS | Completed
STATUS DATE | 11/11/2024
ACTIVITY CODE | 4G.026

Objectives

  • To conduct a system level concept analysis to make sure the DC/DC concept fits the most common product needs.

  • To explore the possibilities and drawbacks with digital controlled DC/DC converters

  • To explore potential from new technologies such as GaN devices

  • To design and test a bread board to evaluate the performance

Challenges

To implement digital control “from scratch” and make it a competitive alternative to traditional analog control.

System Architecture

The architecture consists of a centralized microcontroller that controls three independent DC/DC-converter simultaneously.

Plan

  • First step is a conceptual design to be specified and defined.

  • Second step is to have a BB design Review.

  • Third step is to complete all tests and relevant analysis as input to the final review

Current Status

The project is completed