Mr Zaccheo Nicola (SITAEL)
6/14/17, 9:30 AM
Nicola Zaccheo, Chief Executive Officer at SITAEL S.p.A. welcomes participants.
Mrs Angela Caporale (SITAEL)
6/14/17, 9:45 AM
Mr Gianluca Furano (ESA/Data Systems Division)
6/14/17, 9:55 AM
Mr Olivier Notebaert (Airbus Defence and Space)
6/14/17, 10:05 AM
Mr Alberto Valverde Carretero (ESA), Mr Luca Bolognino (ESA)
6/14/17, 11:10 AM
Presentation will focus on the already important CAN heritage at ESA, showing timeline of past, current and future CAN-powered ESA missions.
Mr Stephane Cael (Thales)
6/14/17, 11:35 AM
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...
Mr Jean Dalenq (Airbus Defence and Space)
6/14/17, 12:05 PM
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.
Mr Carsten Siemers (OHB)
6/14/17, 12:35 PM
Mr Ferrarese Filippo (VECTOR)
6/14/17, 2:00 PM
Outlook on the current status of Vector main tools for the analysis, simulation and testing of CAN/CAN-FD networks
Mrs Laura Boi (Thales Alenia Space)
6/14/17, 2:45 PM
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.
Mr Pietro Tosi (SITAEL)
6/14/17, 3:15 PM
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...
Mrs Emily Crudo (ESA/ESTEC)
6/14/17, 4:15 PM
Mr Lorenzo Gonzales (Skylabs)
6/14/17, 4:45 PM
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...
Mr Bruno Storni (ADELSY)
6/14/17, 5:10 PM
Mr Alfredo Torre (SITAEL)
6/14/17, 5:50 PM
6/14/17, 6:05 PM
Dr Holger Zeltwanger (CIA - CAN in Automation)
6/15/17, 9:00 AM
In 1992 Holger founded the international users’ and manufacturers’ group CAN in Automation (CiA). To this date he is General Manager of CiA.
Dr Maurizio Caramia (Thales Alenia Space)
6/15/17, 10:15 AM
Mr Marco Rovatti (ESA-ESTEC)
6/15/17, 10:50 AM
Mr Christoph Schieber (TESAT Gmbh)
6/15/17, 11:50 AM
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...
Mr Giovanni D’Aliesio (MDA)
6/15/17, 12:25 PM
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...
Dr Giuseppe Montano (Airbus Defence and Space Ltd)
6/15/17, 2:00 PM
26. Performance of CAN protocol for Space based on its use on Raman Laser Spectrometer for Exomars Mission
Mrs Laura Seoane Purrinos (INTA)
6/15/17, 2:30 PM
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...
Mr Oscar Mansilla (Intersil)
6/15/17, 2:55 PM
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 to...
Mr Narayanan Sriram
6/15/17, 3:25 PM
Ms Gonsalves Elaine (Cobham-Aeroflex)
6/15/17, 4:25 PM
Mr Volodymyr Burkhay (SPACE IC GmbH)
6/15/17, 4:55 PM
Mr Luca Bolognino (ESA/ESTEC)
6/15/17, 5:20 PM
Mr Danilo Rubini (Agenzia Spaziale Italiana), Mr Roberto Formaro (Agenzia Spaziale Italiana)
6/16/17, 9:00 AM
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...
Mr Nicolas Ganry (ATMEL/Microchip)
6/16/17, 9:40 AM
The talk will deal with the CAN protocol presentation, the CAN bus native securities for space and the Microchip /Atmel CAN for space.
Mrs Gonsalves Elaine (Cobham)
6/16/17, 10:10 AM
Mr Dejan Gacnik (SkyLabs d.o.o.)
6/16/17, 11:10 AM
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...
Mr Sandi Habinc (Aeroflex Gaisler AB)
6/16/17, 11:40 AM
Mr Jean-Brieuc Feron (SABCA), Mr Marco Ruiz (SABCA)
6/16/17, 12:10 PM
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...
Mr Artur Scholz (ESOC)
6/16/17, 12:35 PM
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...
Mr Alessandro Avanzi (SITAEL)
6/16/17, 2:00 PM
Mr Raffaello Secondo (CERN)
6/16/17, 2:25 PM