THE ECSS PACKET UTILIZATION STANDARD AND ITS SUPPORT TOOL - PowerPoint PPT Presentation

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THE ECSS PACKET UTILIZATION STANDARD AND ITS SUPPORT TOOL

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Standardization of spacecraft monitoring and control. Improvements ... Trailer. Secondary. Header. CCSDS = Overall packet structure. ECSS PUS = Packet content ... – PowerPoint PPT presentation

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Title: THE ECSS PACKET UTILIZATION STANDARD AND ITS SUPPORT TOOL


1
THE ECSS PACKET UTILIZATION STANDARD AND ITS
SUPPORT TOOL
  • Mario Merri - ESA/ESOC
  • Bryan Melton, Serge Valera - ESA/ESTEC
  • Andrew Parkes - Nova Space Associates Ltd

2
Agenda
  • Introduction
  • Standardization of spacecraft monitoring and
    control
  • Improvements and extensions to the ESA PUS
  • The PUS tailoring and supporting tool
  • Conclusions

3
What is the PUS?
  • It is a standard that complements the CCSDS
    packet TM TC recommendations by defining the
    application-level interface between ground and
    space
  • It covers nominal, contingency and
    troubleshooting operations for both AIV and
    mission operations
  • It provides operational concepts and a set of
    on-board services meeting them
  • It defines TM TC packets (including structures)
    to exploit the on-board services
  • It promotes the selection and tailoring of the
    on-board services according to the needs of a
    given mission
  • It allows mission-specific extensions

4
History and Status of PUS
  • PUS Issue 1 published as an ESA standard
    (PSS-07-101) in May 1994
  • at that time, in Europe, only the EURECA mission
    used packet TM TC
  • ECSS Working Group E-70 (Ground Systems and
    Operations) took over PUS and revised it
  • feedback from missions that have used the PUS
  • studies have applied/validated the PUS
  • many review comments collected
  • need to align with latest CCSDS work
  • ECSS PUS status
  • public review closed on 1 June 2001
  • waiting for ECSS final approval and publication

5
Missions Using or Considering the PUS
  • XMM
  • MSG
  • INTEGRAL
  • GOMOS (Envisat Instrument)
  • ATV
  • Ørsted (Danish microsatellite)
  • PROBA
  • ROSETTA
  • MARS EXPRESS
  • HERSCHEL-PLANK
  • CRYOSAT
  • GOCE
  • GALILEO

Virtually all future ESA missions are considering
to adopt the PUS
6
Why PUS?
  • GOAL reduce costs and risks of developing and
    operating on-board and ground systems and provide
    interoperability capability
  • APPROACH re-use/share experience (ops concept)
    and software by
  • standardise the spacecraft operational concept
  • generalise the spacecraft on-board architecture
  • standardise the service model
  • standardise MC messages as a direct consequence
    of the underlying service model (and not the
    other way around)

7
The PUS Standardisation Approach
Generic Operations Concept
Generic On-Board Architecture
Generic Service Model
Message Definition
  • Generic common across missions of different
    nature (scientific, microgravity, etc.) and
    orbital profile (interplanetary, low-Earth,
    geostationary, etc.)

8
Generic Operations Concept
  • Operations concepts include
  • Concepts relating to routine operations
    scenarios, such as telecommanding and telecommand
    verification, telemetry reporting, on-board
    software management, on-board operations
    scheduling, on-board monitoring, on-board storage
    and retrieval and packet forwarding control
  • Concepts that relate to non-routine operations
    scenarios, such as software and memory
    maintenance and troubleshooting, diagnostic data
    reporting and off-line testing
  • Not all of the operation concepts are necessarily
    applicable to a given mission

9
Generic On-Board Architecture
  • Minimal assumptions on on-board architecture
    based on the concept of Application Process (AP)
  • An AP, uniquely identified by an APID, is a
    system element capable of generating TM packets
    and receiving TC packets
  • An AP can control other system elements (e.g.
    memory, device, on-board schedule, etc.)
  • An AP can be implemented in software, firmware or
    hardware.
  • No restrictions on the mapping between APs and
    the usual functional subdivision of a satellite
    into sub-systems and payloads
  • A microprocessor can host one or more APs. An AP
    (presumably a rather complex one) can be
    distributed across two or more microprocessors
  • Standardised messages are exchanged between
    ground and on-board APs that are independent of
    the transfer method
  • currently via CCSDS TM and TC packets
  • but open to other technologies (e.g. TCP/IP)

On-board Application Processes
TM Source Packets
TC Packets
Ground Service Users
10
Generic (Standard) Service Model
1 Telecommand Verification 2 Device Command
Distribution 3 Housekeeping and Diagnostic Data
Reporting 4 Parameter Statistics
Reporting 5 Event Reporting 6 Memory
Management 8 Function Management 9 Time Management
11 On-board Operations Scheduling 12 On-board
Monitoring 13 Large Data Transfer 14 Packet
Forwarding Control 15 On-board Storage and
Retrieval 17 Test 18 On-board Operations
Procedure 19 Event/Action
Commonality needed by several missions Coherence
self contained Implementation independent
minimal assumptions on on-board
architecture Minimum set core functionality of a
mission control system and electrical ground
support equipment
11
Message Definition
  • ESA wants to be compliant to CCSDS Packet TM and
    TC, but there are many ways to use packets!
  • To achieve full standardisation one needs to
    define
  • the information exchange operational protocol
  • the information to be exchanged (messages)
  • the information format and structures
  • the information tailorability for a given
    mission

12
IMPROVEMENTS AND EXTENSIONS TO THE ESA PUS (1)
  • Alignment with evolution of CCSDS recommendations
  • CCSDS removal of TM Segmentation concept releases
    Grouping Flags for use by Application Processes
  • CCSDS File Transfer Protocol considered as
    complementary to PUS
  • PUS Large Data Transfer Service retained as it
    affords a more secure mechanism for conveying a
    series of packets than using the segmentation
    flags
  • Improvements in structure and presentation
  • removed operational requirements
  • added underlying operational concepts
  • provided guidelines for commonly-asked questions
  • emphasised tailoring concept
  • Clarified scope of services and removed
    ambiguities

13
IMPROVEMENTS AND EXTENSIONS TO THE ESA PUS (2)
  • Modifications to the Scope of the PUS
  • Packet Header/Data Field Header
  • added optional Type/Sub-type counter in TM Data
    Field Header
  • added optional Source and Destination IDs in TC
    and TM Data Field Headers, respectively
  • Services
  • added 2 new services On-Board Operations
    Procedure and Event/Action
  • merged Time Management and Time Reporting
    services
  • merged Function Management and Task Management
    services
  • extended On-board Storage and Retrieval service
    (on-board store catalogue and 2 options for the
    downlinking of retrieved packets)
  • added option for both the On-board Storage and
    Retrieval service and the Packet Forwarding
    Control service to be implemented either in a
    distributed manner or to be provided by a
    centralised Application Process
  • defined standard TC verification failure codes
    (based on XMM, MSG, Rosetta)

14
PUS Tailoring Concept
New a prototype tool available to automate PUS
tailoring and generation of mission-specific PUS
document
The specification of the standard services
identifies different levels at which each service
can be implemented, ranging from a very basic
functionality through to the most complex level
PUS Standard
PUS Services Tailoring
PUS Service selection
On-board Ground Segment Implementations
  • Operations Concept
  • Operational Requirements
  • Spacecraft Design
  • Ground Segment Design

15
Conclusions
  • ESA PUS has been revised on the basis of
    real-life experience
  • Operational concept and messages are fully mature
    (started about 10 years ago) and have been
    validated on real spacecraft and systematically
    used for new missions
  • This already brings significant cost and risk
    reduction in the development and operations of
    both space and ground systems
  • ESA ground infrastructure is ready (SCOS-2000)
  • The new ECSS PUS will be soon available and will
    further establish the PUS as The Standard in
    this field
  • The availability of tools will facilitate the
    tailoring of the PUS to missions
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