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Operational Flight Dynamics
CNES Toulouse, France
Monique MOURY
Monique.moury@cnes.fr
Hyattsville, SSA 2015
May 12, 2015
CNES role in
French Space Surveillance
SUMMARY
SSA 2015 – French SSA2
 MITIGATION
 OPERATIONAL ACTIVITIES
 FOCUS on COLLISION AVOIDANCE
SSA 2015- French SSA3
SPACE DEBRIS MITIGATION
French Space Act – JUNE 2008
Objective:
 To authorize and to monitor space activities when
France bears international responsibility
Shall obtain an authorization since DEC 10:
 Any operator launching or controlling a space object from French territory or French
facilities
 Any French operator launching a space object from anywhere
 Any French operator controlling a space object in orbit
Authorizations are granted by the Ministry in charge of space
based on:
 Administrative review of the main characteristics of the company
 Technical review: compliance to the Technical Regulations is checked by CNES on
behalf of the Ministry in charge of space
SSA 2015- French SSA4
Objective => protection of:
People
Public health
Properties
Environment on Earth, in Atmosphere or in Orbit
Directly derived from ISO 24113
Compliant with IADC and UN-COPUOS Mitigation Guidelines
A 10-year transition period is foreseen (2010 – 2020)
During this period, some of the requirements may be not fulfilled: the operator
shall demonstrate that best efforts have been accomplished taking in account
the existing design
After the transition period all the requirements will be mandatory
SPACE DEBRIS MITIGATION
Technical Regulations
SSA 2015- French SSA5
SPACE SURVEILLANCE
French Organization
Overall responsibility belongs to Defense
CIE: « Commandement Interarmées de l’Espace », Joint Space Command
Air Force
Operational organization is shared between Air Force and CNES
Air Force and Procurement Agency (Defense)
Overall coordination
Operation of the surveillance system (GRAVES)
Operation of the tracking radars
CNES (Research and Defense)
Station keeping of civilian and military satellites
In-orbit collision risk monitoring
Launch collision risk monitoring
Prediction of atmospheric reentries
Flight dynamics support to Air Force
Implementation of French Space Act
SSA 2015- French SSA6
OPERATIONAL ACTIVITIES
at CNES
Maintenance of a catalog of orbits of LEO objects using GRAVES data
Altitude < 1000 km
35° < inclination < 145°
Launch collision avoidance
French Space Act requires to take into account human space flights
In-orbit collision avoidance
Service delivered to all satellites controlled at CNES and open to external satellites
Middle Man between Conjunction Message provider and operators
End of life operations
Transition phase for French Space Act requirements
Atmospheric re-entry predictions
SSA 2015- French SSA7
OPERATIONAL ACTIVITIES
Launch Collision Avoidance
Input data :
 Launched objects trajectory and dispersion (primary objects)
 manned vehicles trajectory and dispersion (secondary objects)
 Closing window criteria
Output data : Closed instants in the launch window to avoid the collision
risk
Launch window0 3600 s
Closed instants
SSA 2015- French SSA8
OPERATIONAL ACTIVITIES
End of life operations
30 years of improvements for end of life operations at CNES
GEOSTATIONARY SATELLITES (since 1975)
Symphonie : get out of the GEO ring
Telecom 1 : complete reorbitation
TDF : fluidic passivation
Telecom 2 : reliability
 REMOTE SENSING SATELLITES (since 1985)
Spot 1, 2 : lowering perigee
Helios 1, SPOT 4 : fluidic passivation
Spot 5, Helios 2, Pleiades : preparing the future
 MINI & MICRO SATELLITES (since 2000)
Essaim : multiple disposal
Demeter : fluidic passivation
Parasol & Jason 1 : get out of operational orbit
SSA 2015- French SSA9
OPERATIONAL ACTIVITIES
End of life operations : synthesis
CNES has controlled 39 satellites since 40 years
… and has performed EOL operations for more than half of them
 Many improvements, mainly concerning passivation and automation
Still a lot to be done…
17 : nominal operations,
1 : anticipated operations due to a payload component failure
2 : removed from operational orbit before end of life, to reduce risk towards
other satellites in case of failure : it proved a wise decision for one of them.
2 : emergency situation, successfully handled
2 : lost with no possible disposal operations
Through end of life operations and collision risk management, satellite
operators contribute to prevent significant causes of space debris generation
SSA 2015- French SSA10
OPERATIONAL ACTIVITIES
Atmospheric re-entry predictions
Objectives of the monitoring process:
Detect objects representing a risk to French territory
Detect French registered objects representing a risk to foreign
countries
Main steps:
Long term:
» Automatic screening of the catalogue, filtering based on perigee altitude
» Ballistic coefficient estimation and lifetime determination
Middle term (<2 months)
» Orbit monitoring with dedicated CNES tool OPERA
» Object characteristics and, when possible, fragmentation analysis
» Risk computation
Short term (< 3 days)
» Tracking measurements, reentry prediction with uncertainties
» On-ground track
» Risk update
SSA 2015- French SSA11
ORERATIONAL ACTIVITIES
In-orbit Collision Avoidance is essential
2007 January 11th : Old Fengyun 1C satellite is deliberately destroyed by a
missile (ASAT)
=> Debris cloud of 2 000 cataloged objects
2009 February 10th : Operational Iridium 33 satellite collides with Cosmos
2251 satellite (not operational since 1995)
=> 2 debris clouds of respectively 600 and 1 600 cataloged objects
Impact of those 2 “events” => ~50% of the detected close approaches in LEO
involve a debris from one of those 3 clouds
The Iridium – Cosmos collision
could have been avoided...
SSA 2015- French SSA12
Conjunction Assessment
Conjunction Messages: a real satellite protection …
Since 2009, JSpOC distributes conjunction messages
to all satellite owners/operators (O/O)
As a positive
reaction to this
situation …
O/O O/O O/O O/O O/O O/O …
JSpOC
SSA 2015- French SSA13
Orbit Determination
characteristics
Conjunction message, an information message
=
Conjunction Summary Message since July 2010
Position/Velocity
Position dispersion
Time of the Closest Approach
Conjunction Assessment
CSM: what is it ?
SSA 2015- French SSA14
Conjunction message, an information message
=
Conjunction Data Message since April 2014
Conjunction Assessment
CDM: what is it ?
SSA 2015- French SSA15
O/O must put in place an
Acquisition, Evaluation, Alert and
Recommendation process:
 Automatic acquisition : 24/7
Risk Evaluation:
Alert FD team of the Control Center
Recommendation for avoidance
Only very few CMs lead to an
avoidance action, but those messages
(HIE) mustn’t be missed.
 This process is not so easy …
Middle Man Concept
Conjunction Assessment is a two-step process
Space Surveillance Network
JSpOC
Precise complete catalog
Screening – Information Messages generation
Avoid… the avoidable
SSA 2015- French SSA16
O/O
JSpOC
Ephem.
CAESAR
Conjunction Analysis and Evaluation Service : Alerts and Recommendations
Flight Dynamics
System
(SPADOC)
Flight Dynamics
System (X)
ΔV
ΔV
CASR
JWD = CAESAR
WARN ALERT
Flight Dynamics
System (JOCC)
On Call analyst
On Call analyst
JWD = Analyst
On Call O/O
JWD = O/O
CDMs-JSPOC
CDMs-ALM
CDMs-GNOSE
GO
TC
ΔV
ΔV
Screening
additional
measurement (when
available)
Almanac
Improved OD
ΔV
SSA 2015- French SSA17
Java for Assessment of Conjunctions
JAC contributes to the collaborative work environment for CAESAR.
 JAC addresses the needs of teams responsible for managing in-orbit collision
risks for one or many satellites.
 JAC helps to retrieve and analyze close approach alerts by providing a synthetic
vision of each close approach described by CDMs. It helps the user to evaluate
the level of risk according to its own criteria and to take and validate a decision.
 JAC is a modular software :
 JAC Basic Module: to be aware of the situation.
 JAC Expert Module: to take and validate a decision.
JAC is distributed by CNES after signature of a license
SSA 2015- French SSA18
In-orbit Collision Avoidance
Synthesis
 JSpOC’s CDMs combined with O/O data thanks to Middle Man entities are the best available
data to avoid collision in space:
All the O/O should take into account JSpOC’s CDMs: but it is not an easy process;
The Middle Men can help O/O and improve the reliability of the process;
Reliability of the process protects space environment for the benefit of all, but does not guarantee
individual satellite protection => public role (for ex European Commission decision for EU service)
CAESAR (the French Middle Man) relies on JAC software for its essential collaborative work
environment.
 Some of the difficulties of CA:
 Take into account maneuvers => LARGE CRITERIA
 Deal with huge amount of CDMs => BURDEN-SHARING BETWEEN JSpOC & Middle Man
 Risk level sensitivity to small variations of input data => EXPANDED PoC
 JAC, distributed by CNES in 2 levels, can help:
Basic (“to be aware of the situation”) for free;
Expert (“to take and validate a decision”) for an annual fee.
https://spod.cnes.fr
jac@cnes.fr

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Space Situational Awareness Forum - CNES Presentation

  • 1. Operational Flight Dynamics CNES Toulouse, France Monique MOURY Monique.moury@cnes.fr Hyattsville, SSA 2015 May 12, 2015 CNES role in French Space Surveillance
  • 2. SUMMARY SSA 2015 – French SSA2  MITIGATION  OPERATIONAL ACTIVITIES  FOCUS on COLLISION AVOIDANCE
  • 3. SSA 2015- French SSA3 SPACE DEBRIS MITIGATION French Space Act – JUNE 2008 Objective:  To authorize and to monitor space activities when France bears international responsibility Shall obtain an authorization since DEC 10:  Any operator launching or controlling a space object from French territory or French facilities  Any French operator launching a space object from anywhere  Any French operator controlling a space object in orbit Authorizations are granted by the Ministry in charge of space based on:  Administrative review of the main characteristics of the company  Technical review: compliance to the Technical Regulations is checked by CNES on behalf of the Ministry in charge of space
  • 4. SSA 2015- French SSA4 Objective => protection of: People Public health Properties Environment on Earth, in Atmosphere or in Orbit Directly derived from ISO 24113 Compliant with IADC and UN-COPUOS Mitigation Guidelines A 10-year transition period is foreseen (2010 – 2020) During this period, some of the requirements may be not fulfilled: the operator shall demonstrate that best efforts have been accomplished taking in account the existing design After the transition period all the requirements will be mandatory SPACE DEBRIS MITIGATION Technical Regulations
  • 5. SSA 2015- French SSA5 SPACE SURVEILLANCE French Organization Overall responsibility belongs to Defense CIE: « Commandement Interarmées de l’Espace », Joint Space Command Air Force Operational organization is shared between Air Force and CNES Air Force and Procurement Agency (Defense) Overall coordination Operation of the surveillance system (GRAVES) Operation of the tracking radars CNES (Research and Defense) Station keeping of civilian and military satellites In-orbit collision risk monitoring Launch collision risk monitoring Prediction of atmospheric reentries Flight dynamics support to Air Force Implementation of French Space Act
  • 6. SSA 2015- French SSA6 OPERATIONAL ACTIVITIES at CNES Maintenance of a catalog of orbits of LEO objects using GRAVES data Altitude < 1000 km 35° < inclination < 145° Launch collision avoidance French Space Act requires to take into account human space flights In-orbit collision avoidance Service delivered to all satellites controlled at CNES and open to external satellites Middle Man between Conjunction Message provider and operators End of life operations Transition phase for French Space Act requirements Atmospheric re-entry predictions
  • 7. SSA 2015- French SSA7 OPERATIONAL ACTIVITIES Launch Collision Avoidance Input data :  Launched objects trajectory and dispersion (primary objects)  manned vehicles trajectory and dispersion (secondary objects)  Closing window criteria Output data : Closed instants in the launch window to avoid the collision risk Launch window0 3600 s Closed instants
  • 8. SSA 2015- French SSA8 OPERATIONAL ACTIVITIES End of life operations 30 years of improvements for end of life operations at CNES GEOSTATIONARY SATELLITES (since 1975) Symphonie : get out of the GEO ring Telecom 1 : complete reorbitation TDF : fluidic passivation Telecom 2 : reliability  REMOTE SENSING SATELLITES (since 1985) Spot 1, 2 : lowering perigee Helios 1, SPOT 4 : fluidic passivation Spot 5, Helios 2, Pleiades : preparing the future  MINI & MICRO SATELLITES (since 2000) Essaim : multiple disposal Demeter : fluidic passivation Parasol & Jason 1 : get out of operational orbit
  • 9. SSA 2015- French SSA9 OPERATIONAL ACTIVITIES End of life operations : synthesis CNES has controlled 39 satellites since 40 years … and has performed EOL operations for more than half of them  Many improvements, mainly concerning passivation and automation Still a lot to be done… 17 : nominal operations, 1 : anticipated operations due to a payload component failure 2 : removed from operational orbit before end of life, to reduce risk towards other satellites in case of failure : it proved a wise decision for one of them. 2 : emergency situation, successfully handled 2 : lost with no possible disposal operations Through end of life operations and collision risk management, satellite operators contribute to prevent significant causes of space debris generation
  • 10. SSA 2015- French SSA10 OPERATIONAL ACTIVITIES Atmospheric re-entry predictions Objectives of the monitoring process: Detect objects representing a risk to French territory Detect French registered objects representing a risk to foreign countries Main steps: Long term: » Automatic screening of the catalogue, filtering based on perigee altitude » Ballistic coefficient estimation and lifetime determination Middle term (<2 months) » Orbit monitoring with dedicated CNES tool OPERA » Object characteristics and, when possible, fragmentation analysis » Risk computation Short term (< 3 days) » Tracking measurements, reentry prediction with uncertainties » On-ground track » Risk update
  • 11. SSA 2015- French SSA11 ORERATIONAL ACTIVITIES In-orbit Collision Avoidance is essential 2007 January 11th : Old Fengyun 1C satellite is deliberately destroyed by a missile (ASAT) => Debris cloud of 2 000 cataloged objects 2009 February 10th : Operational Iridium 33 satellite collides with Cosmos 2251 satellite (not operational since 1995) => 2 debris clouds of respectively 600 and 1 600 cataloged objects Impact of those 2 “events” => ~50% of the detected close approaches in LEO involve a debris from one of those 3 clouds The Iridium – Cosmos collision could have been avoided...
  • 12. SSA 2015- French SSA12 Conjunction Assessment Conjunction Messages: a real satellite protection … Since 2009, JSpOC distributes conjunction messages to all satellite owners/operators (O/O) As a positive reaction to this situation … O/O O/O O/O O/O O/O O/O … JSpOC
  • 13. SSA 2015- French SSA13 Orbit Determination characteristics Conjunction message, an information message = Conjunction Summary Message since July 2010 Position/Velocity Position dispersion Time of the Closest Approach Conjunction Assessment CSM: what is it ?
  • 14. SSA 2015- French SSA14 Conjunction message, an information message = Conjunction Data Message since April 2014 Conjunction Assessment CDM: what is it ?
  • 15. SSA 2015- French SSA15 O/O must put in place an Acquisition, Evaluation, Alert and Recommendation process:  Automatic acquisition : 24/7 Risk Evaluation: Alert FD team of the Control Center Recommendation for avoidance Only very few CMs lead to an avoidance action, but those messages (HIE) mustn’t be missed.  This process is not so easy … Middle Man Concept Conjunction Assessment is a two-step process Space Surveillance Network JSpOC Precise complete catalog Screening – Information Messages generation Avoid… the avoidable
  • 16. SSA 2015- French SSA16 O/O JSpOC Ephem. CAESAR Conjunction Analysis and Evaluation Service : Alerts and Recommendations Flight Dynamics System (SPADOC) Flight Dynamics System (X) ΔV ΔV CASR JWD = CAESAR WARN ALERT Flight Dynamics System (JOCC) On Call analyst On Call analyst JWD = Analyst On Call O/O JWD = O/O CDMs-JSPOC CDMs-ALM CDMs-GNOSE GO TC ΔV ΔV Screening additional measurement (when available) Almanac Improved OD ΔV
  • 17. SSA 2015- French SSA17 Java for Assessment of Conjunctions JAC contributes to the collaborative work environment for CAESAR.  JAC addresses the needs of teams responsible for managing in-orbit collision risks for one or many satellites.  JAC helps to retrieve and analyze close approach alerts by providing a synthetic vision of each close approach described by CDMs. It helps the user to evaluate the level of risk according to its own criteria and to take and validate a decision.  JAC is a modular software :  JAC Basic Module: to be aware of the situation.  JAC Expert Module: to take and validate a decision. JAC is distributed by CNES after signature of a license
  • 18. SSA 2015- French SSA18 In-orbit Collision Avoidance Synthesis  JSpOC’s CDMs combined with O/O data thanks to Middle Man entities are the best available data to avoid collision in space: All the O/O should take into account JSpOC’s CDMs: but it is not an easy process; The Middle Men can help O/O and improve the reliability of the process; Reliability of the process protects space environment for the benefit of all, but does not guarantee individual satellite protection => public role (for ex European Commission decision for EU service) CAESAR (the French Middle Man) relies on JAC software for its essential collaborative work environment.  Some of the difficulties of CA:  Take into account maneuvers => LARGE CRITERIA  Deal with huge amount of CDMs => BURDEN-SHARING BETWEEN JSpOC & Middle Man  Risk level sensitivity to small variations of input data => EXPANDED PoC  JAC, distributed by CNES in 2 levels, can help: Basic (“to be aware of the situation”) for free; Expert (“to take and validate a decision”) for an annual fee. https://spod.cnes.fr jac@cnes.fr