Conveners
CAN bus in Space - Session 2: CAN In Space - Applications
- Chris Taylor (ESA/Data Systems Division)
- Gianluca Furano (ESA - ESTEC - TEC-EDD)
- Giorgio Magistrati (ESA/Data Systems Division)
Description
Continuation of Session 1 with industry's position papers, presenattion of CAN tools and wrap up discussions.
Mr
Giorgio Magistrati
(ESA/Data Systems Division)
23/10/2013, 09:00
CAN Bus in Space (22 October PM & 23 October AM)
Mr
Alberto Valverde Carretero
(ESA/Data Systems Division)
23/10/2013, 09:10
CAN Bus in Space (22 October PM & 23 October AM)
The modularity of the ECSS CAN standard based on CANOpen opens a wide range of possibilities in terms of HW/SW partitioning schemes in its implementation. The standard can be fully implemented in HW (i.e. CCIPC and RCCIPC), fully implemented in SW using existing CANOpen stacks or anything in between. This presentation and the associated demo will analyze different scenarios, with different...
Mr
Luca Fossati
(ESA/Data Systems Division)
23/10/2013, 09:20
CAN Bus in Space (22 October PM & 23 October AM)
ESA/ESTEC maintains and distributes under ESA licenses a small catalogue of IP Cores which comprise typical digital functions used in space applications.The ESA IP cores can be licensed for space research and/or commercial use,under specific conditions (depending on the IP ownership) to companies basedin ESA member and participant states.This talk will focus mostly on two of the IP-Cores...
Mr
Frédéric Vidy
(Vector)
23/10/2013, 09:30
CAN Bus in Space (22 October PM & 23 October AM)
The idea of the CAN bus is getting 30 years old in 2013. Within this time the CAN bus has not only established itself as the standard communication protocol in automotive networks but is also in use in aerospace or industrial applications. Although there are also other bus systems used in these areas, the CAN bus will still keep its strong market position for quite a while. With the CAN-FD...
Mr
Jan Andersson
(Aeroflex Gaisler)
23/10/2013, 10:10
CAN Bus in Space (22 October PM & 23 October AM)
The Controller Area Network (CAN) was initially created for automotive applications as a method for enabling robust serial communication. The CAN bus was identified by the European Space Agency (ESA) as a possible replacement for the On-Board Data Handling (OBDH) bus in the late '90s, with the SMART-1 satellite as the first successful example of its usage in an ESA mission. Although the OBDH...
Mr
Vangelis Kollias
(TELETEL SA)
23/10/2013, 10:25
CAN Bus in Space (22 October PM & 23 October AM)
Presentation of the Protocol Validation System (PVS) by TELETEL, which is a new generation EGSE SCOE, already supporting SpaceWire and MIL-STD-1553, being now extended to support CAN. PVS can be used for rapid prototyping & evaluation of new network protocols/features, for interface simulation, functional testing and stress testing. Moreover it can be used for device simulation (SSMM, RTU,...
Mr
Jean Dalenq
(Astrium)
23/10/2013, 11:05
CAN Bus in Space (22 October PM & 23 October AM)
Presentation
A successful CAN bus for telecom payload needs to fulfill precisely the extreme satcom requirements: high reliability of electronic components, high availability of the system solution achieved by minor modifications of the system architecture. Considering all those constraints, physical layer, redundancy management and protocol have been tailored to define a robust, efficient and cheap CAN...
Mr
Maurizio Caramia
(Thales Alenia Space)
23/10/2013, 11:25
CAN Bus in Space (22 October PM & 23 October AM)
Presentation
This paper presents the on-going activities and solutions related to the development, research and standardization processes of the CAN Bus solutions carried out in the EXOMARS projects and studies where Thales Alenia Space Italy (TAS-I) is leading the industrial activities in collaboration with the European Space Agency.
The CAN communication bus has been successfully used for many years in...
Mr
Jacques Busseuil
(Thales Alenia Space)
23/10/2013, 11:45
CAN Bus in Space (22 October PM & 23 October AM)
The objective of this activity is the development of a ‘CAN solution’ to be used in platform and payload avionics of telecom satellites. The proposed CAN solution has to cover all the aspects related to the introduction of the CAN bus in telecom satellites, from the physical and protocol layer definition up to the test and validation procedure definition.
A breadboard system fully ...
Mr
Francesco Ortix
(Temis)
23/10/2013, 12:00
CAN Bus in Space (22 October PM & 23 October AM)
The suite of CAN bus and protocols has been developed to create a reliable, safety critical, deterministic time communication over automotive electronic box use for the complete management of stock cars. It has been demonstrated over time and by widespread diffusion on automotive market the effectiveness and efficiency of CAN protocol and electrical bus on safety critical systems (ABS...
Mr
David Stanton
(SSTL)
23/10/2013, 12:20
CAN Bus in Space (22 October PM & 23 October AM)
SSTL have been using CAN bus as their primary method of transferring commands and telemetry around their spacecraft of over a decade. The use of CAN bus is at the heart of their nominal and non-nominal concept of operations. The architecture allows complete access to spacecraft systems by the ground segment independent of the spacecraft onboard computer to allow versatile strategies for...
Mr
Chris Taylor
(ESA/Data Systems Division), Mr
Gianluca Furano
(ESA/Data Systems Division), Mr
Giorgio Magistrati
(ESA/Data Systems Division)
23/10/2013, 12:40
CAN Bus in Space (22 October PM & 23 October AM)
Wrap up round table.
