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14-16 June 2017
Europe/Rome timezone
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Contribution List

Displaying 37 contributions out of 37
Presented by Ms. Gonsalves ELAINE on 15 Jun 2017 at 16:25
Intersil released the first to market class V radiation hardened CANbus transceiver family in March of 2016. The basic features and performance of the transceivers in this family will be presented. We will introduce our new “A” version family of CAN transceivers that were release in April 2017. The “A” versions transceivers, when configured in the medium speed mode, supports data rates up ... More
Presented by Mr. Oscar MANSILLA on 15 Jun 2017 at 14:55
An overview of CAN bus applications within Airbus Defence and Space will be presented and for each application the main characteristics of the network will be described. Main part of the presentation is focused on Telecom.
Presented by Mr. Jean DALENQ on 14 Jun 2017 at 12:05
MDA's space electronics division located in Montreal, Canada, has been designing, manufacturing and testing complex electronic sub-systems for space missions over the past 40 years. These include platform and payload computers and avionics suites, motor control, data storage and digital signal processing, as well as RF electronics and power converters. MDA has significant heritage in implementing ... More
Presented by Mr. Giovanni D’ALIESIO on 15 Jun 2017 at 12:25
Presented by Mr. Carsten SIEMERS on 14 Jun 2017 at 12:35
Tesat-Spacecom is an equipment supplier for telecommunication payloads. Therefore the presentation covers the application of CAN in the different products of Tesat-Spacecom. The presentation will cover aspects of interface standardization due to the use of the CAN interface as well as implementation details. Furthermore some technical challenges of CAN application are pointed out and a short outlo ... More
Presented by Mr. Christoph SCHIEBER on 15 Jun 2017 at 11:50
In 1992 Holger founded the international users’ and manufacturers’ group CAN in Automation (CiA). To this date he is General Manager of CiA.
Presented by Dr. Holger ZELTWANGER on 15 Jun 2017 at 09:00
Presentation will focus on the already important CAN heritage at ESA, showing timeline of past, current and future CAN-powered ESA missions.
Presented by Mr. Luca BOLOGNINO, Mr. Alberto VALVERDE CARRETERO on 14 Jun 2017 at 11:10
Presentation will be focused on CAN bus at the heart of the TAS avionics architecture and, in particularly, on: - Architecture of CAN bus in THALES ALENIA SPACE design. - Validation strategy of the CAN bus. - CAN validation results: *Electrical tests *Functional tests - Going further / free discussions: *Step forward with integration of the Applicable Document AD919 ... More
Presented by Mr. Stephane CAEL on 14 Jun 2017 at 11:35
The talk will deal with the CAN protocol presentation, the CAN bus native securities for space and the Microchip /Atmel CAN for space.
Presented by Mr. Nicolas GANRY on 16 Jun 2017 at 09:40
The CANopen IP Core (CCIPC) has been developed in the frame of the Exomars project. The CCIPC has been designed to implement the main aspect of the CANopen protocol in order to move from a SW to HW solution and to make all the CAN aspects, from Application to Physical layer, transparent to the final user. This presentation will provide an overview of the main architectural and functional changes ... More
Presented by Mr. Pietro TOSI on 14 Jun 2017 at 15:15
Presented by Mrs. Emily CRUDO on 14 Jun 2017 at 16:15
Presented by Mr. Narayanan SRIRAM on 15 Jun 2017 at 15:25
Presented by Mr. Volodymyr BURKHAY on 15 Jun 2017 at 16:55
For its motor control applications for space vehicles, SABCA developed with ESA support the last member of its processor family : the Control Loop Processor. This deterministic processor is now available for the European space and non-space markets. With its high throughput & precision arithmetic capability, its radiation- & fault-tolerant capability and (between other) its CAN bus communication i ... More
Presented by Mr. Marco RUIZ, Mr. Jean-Brieuc FERON on 16 Jun 2017 at 12:10
Session: E-Bike test ride
on 14 Jun 2017 at 18:05
Presented by Mr. Marco ROVATTI on 15 Jun 2017 at 10:50
Presented by Dr. Maurizio CARAMIA on 15 Jun 2017 at 10:15
Presented by Mr. Gianluca FURANO on 14 Jun 2017 at 09:55
The presentation covers the design of the CAN Application layer used in EXOMARS 2016 Schiaparelli Entry Descent Module, starting from the description of peculiar avionic architecture and functional requirements and ending to performance measurements, and lesson learnt.
Presented by Mrs. Laura BOI on 14 Jun 2017 at 14:45
Presented by Mr. Sandi HABINC on 16 Jun 2017 at 11:40
Autonomous functionality, versatile design, high interoperability between units and shorter time to market are the key aspects of distributed architectural approach. A solution for such highly integrated and distributed design is presented, with basic concept of reusing building blocks on a unit level. Basic building block is represented by flexible and highly configurable, radiation hardened by d ... More
Presented by Mr. Dejan GACNIK on 16 Jun 2017 at 11:10
Session: E-Bike test ride
Presented by Mr. Alfredo TORRE on 14 Jun 2017 at 17:50
Presented by Mr. Olivier NOTEBAERT on 14 Jun 2017 at 10:05
Session: Keynote - III
Mr. Danilo Rubini, Agenzia Spaziale Italiana Head of the Technology Office, part of ASI Technology & Engineering Division; he has been working for the Technology Development Division since 2010, for the Marketing Unit (2004-2010) and previously for the Small and Medium Enterprises Unit (2002-2004). He is National Expert Advisor for ESA Industry Policy Committee (since 2006), National Delegate ... More
Presented by Mr. Roberto FORMARO, Mr. Danilo RUBINI on 16 Jun 2017 at 09:00
Presented by Dr. Giuseppe MONTANO on 15 Jun 2017 at 14:00
Presented by Mr. Luca BOLOGNINO on 15 Jun 2017 at 17:20
Presented by Mrs. Angela CAPORALE on 14 Jun 2017 at 09:45
Presented by Mr. Raffaello SECONDO on 16 Jun 2017 at 14:25
With the ever growing capabilities of FPGAs and microcontrollers, spacecraft systems are evolving from centralized architectures with a single main processing unit to decentralized layouts composed of multiple intelligent nodes. The backbone of this development is the command and control bus that interconnects these units. In this talk we present the details and results of a prototype implementati ... More
Presented by Mr. Artur SCHOLZ on 16 Jun 2017 at 12:35
After previous experiences using CAN in space applications (as interface of some instruments and as main bus in small satellites), INTA (Spanish National Institute for Aerospace Technology) is currently involved in the development of RLS, a Raman Laser Spectrometer to be boarded in ExoMars 2020. RLS is the first implementation at INTA using a standardized high layer (CANOpen based on CCIPC) on top ... More
Presented by Mrs. Laura SEOANE PURRINOS on 15 Jun 2017 at 14:30
With the accelerated development of remote terminal units, there is an increased need for a reliable interface protocol that can be used for communication over CAN. While the CANopen interface protocol is developed for automation and used in variety of terrestrial applications, the ECSS variant implements only a subset of its functionality. As such a CAN interface protocol suitable for use on spac ... More
Presented by Mr. Lorenzo GONZALES on 14 Jun 2017 at 16:45
Presented by Mr. Bruno STORNI on 14 Jun 2017 at 17:10
Outlook on the current status of Vector main tools for the analysis, simulation and testing of CAN/CAN-FD networks
Presented by Mr. Ferrarese FILIPPO on 14 Jun 2017 at 14:00
Nicola Zaccheo, Chief Executive Officer at SITAEL S.p.A. welcomes participants.
Presented by Mr. Zaccheo NICOLA on 14 Jun 2017 at 09:30