From 7a3038707462a9e95b0dec98f545cb962bd7b751 Mon Sep 17 00:00:00 2001
From: Elena.Budnik <ebudnik@irap.omp.eu>
Date: Thu, 3 Nov 2016 14:47:03 +0100
Subject: [PATCH] PEACE

---
 Instrument/AMDA/Cluster-Rumba/PEACE.xml           | 33 ++++++++++++++++++++++++++++-----
 Instrument/AMDA/Cluster-Salsa/PEACE.xml           | 33 ++++++++++++++++++++++++++++-----
 Instrument/AMDA/Cluster-Samba/PEACE.xml           | 34 +++++++++++++++++++++++++++++-----
 Instrument/AMDA/Cluster-Tango/PEACE.xml           | 33 ++++++++++++++++++++++++++++-----
 NumericalData/AMDA/ACE/MFI/ace-mag-real.xml       |  2 +-
 NumericalData/AMDA/ACE/SWEPAM/ace-swepam-real.xml |  2 +-
 6 files changed, 115 insertions(+), 22 deletions(-)

diff --git a/Instrument/AMDA/Cluster-Rumba/PEACE.xml b/Instrument/AMDA/Cluster-Rumba/PEACE.xml
index e6a022b..c489e55 100644
--- a/Instrument/AMDA/Cluster-Rumba/PEACE.xml
+++ b/Instrument/AMDA/Cluster-Rumba/PEACE.xml
@@ -5,22 +5,45 @@
     <ResourceID>spase://CDPP/Instrument/AMDA/Cluster-Rumba/PEACE</ResourceID>
     <ResourceHeader>
       <ResourceName>PEACE</ResourceName>
-      <AlternateName>Plasma Electron and Current Experiment (PEACE)</AlternateName>
-      <ReleaseDate>2011-02-04T15:37:46Z</ReleaseDate>
-      <Description>The primary task of this instrument (PEACE: Plasma Electrons and Currents Experiment) is to obtain the velocity moments of the distribution function of electrons as frequently and as accurately as the spacecraft telemetry will allow. Detector counts are collected in energy, polar-angle, and azimuth-angle bins to form a three-dimensional matrix. Two sensors are used: LEEA (low-energy electron analyzer) and HEEA (high-energy electron analyzer). The energy coverage is from 0.67 eV to 30 KeV in 92 levels. The first 16 levels are equally spaced linearly up to 10.7 eV; the remainder are logarithmically spaced. Both sensors can use the full range, but the HEEA will normally operate over a higher energy range than the LEEA. The LEEA specializes in coverage of the energies from 0.7--10 eV, and has a geometric factor one fifth that of the HEAA. Both sensors consist of hemispherical electrostatic analyzers of the top-hat type and a detector in the form of an annular micro-channel plate with a position-sensitive readout. Each sensor covers the range 0--180 degrees with respect to the spin axis, and they are mounted opposite each other with a view perpendicular to the spin axis, thus covering the complete angular range in a half rotation of the spacecraft. The field of view perpendicular to the fan is 2 degrees for the LEEA and 5.6 degrees for the HEEA. Energy resolution (Delta-E)/E is 0.13 for LEEA and 0.16 for HEEA. There are four sweep modes, synchronized to the spin period (4 s), to vary the azimuthal angular resolution. The spin phasing can be made coincident with that of the CIS instrument, to ensure that the electron and ion moments will be measured simultaneously. On-board processing is used to calculate the moments of the distribution with an accuracy of 1% and to select suitable parts of the complete distribution for transmission. The normal science data format is based on one spin period, and consists of core data followed by other optional distributions as can be fit into the available telemetry for that spin. The core data (moments, spacecraft potential, and pitch angle distribution) are always transmitted (if the spin is nominal). The next distribution is transmitted if, before the end of the spin, all the previous data have been sent. Thus the next spin of data will be transmitted slightly late, but all of its core data will be transmitted before the following spin of data is started on. Eventually the transmission will catch up and be able to transmit the distribution after the core again, but only after some time. This applies at all telemetry rates. The instrument can adapt automatically to six different telemetry rates: a basic 1.52 Kbps rate (CIS priority); a normal 2.52 Kbps rate; an enhanced PEACE priority rate of 3.54 Kbps; and three burst mode rates, with a maximum of 15.98 Kbps. For more details of the Cluster mission, the spacecraft, and its instruments, see the report ``Cluster: mission, payload and supporting activities,'' March 1993, ESA SP-1159, and the included article ``PEACE: a Plasma Electron and Current Experiment,'' by A. D. Johnstone et al., from which this information was obtained.</Description>
+      <AlternateName>Plasma Electron and Current Experiment</AlternateName>
+      <ReleaseDate>2016-11-04T15:37:46Z</ReleaseDate>
+      <Description>
+        The PEACE instrument consists of two sensors, HEEA (High Energy Electron Analyser) and LEEA (Low Energy Electron 
+        Analyser),  and  a  data  processing  unit,  the  DPU.  The  sensors  are  Top  Hat  electrostatic  analysers.  The  basic  measurement 
+        made by PEACE is the  number of counted electrons per accumulation time. The satellite spin period, Tspin
+        , is measured as  the time taken between two detections of the
+        Sun by the  spacecraft sun sensor (which is expected to be 4 seconds ±10%). 
+        Within  the  PEACE  DPU,  the  spin  period  is subdivided  into  1024  equal  parts,  of  duration  Tacc
+        ,  the PEACE accumulation time. The instrument measurement cycle 
+        is thus adjusted to match the spin period so that PEACE collects data from a  full 
+        4pi solid angle (i.e. provides all-sky coverage) during each and every spin. For a nominal 4 second spin, Tacc
+        ~ 3.9 msec.
+        In reality this is calculated from the duration of the previous spin
+        provided by the spacecraft housekeeping.
+      </Description>
+      <Acknowledgement>Principal Investigator: Andrew Fazakerley</Acknowledgement>
       <Contact>
         <PersonID>spase://SMWG/Person/Andrew.N.Fazakerley</PersonID>
         <Role>PrincipalInvestigator</Role>
       </Contact>
       <InformationURL>
+        <Name>ESA web page</Name>
+        <URL>http://sci.esa.int/jump.cfm?oid=33024</URL>
+        <Description>PEACE</Description>
+      </InformationURL>
+      <InformationURL>
         <Name>NSSDC's Master Catalog</Name>
         <URL>http://nssdc.gsfc.nasa.gov/database/MasterCatalog?sc=2000-045A&amp;ex=5</URL>
         <Description>Information about the Plasma Electron and Current Experiment (PEACE) experiment on the Cluster 2/FM5 (Rumba) mission.</Description>
       </InformationURL>
       <PriorID>spase://SMWG/Instrument/Cluster2-Rumba/PEACE</PriorID>
     </ResourceHeader>
-    <InstrumentType>EnergeticParticleInstrument</InstrumentType>
-    <InvestigationName>Plasma Electron and Current Experiment (PEACE) on Cluster 2/FM5 (Rumba)</InvestigationName>
+    <InstrumentType>ElectrostaticAnalyser</InstrumentType>
+    <InvestigationName></InvestigationName>
+    <OperatingSpan>
+      <StartDate>2000-12-01T00:00:00</StartDate>
+      <Note>Start of full orbit coverage: 2002-06-01T00:00:00</Note>
+    </OperatingSpan>
     <ObservatoryID>spase://CDPP/Observatory/AMDA/Cluster-Rumba</ObservatoryID>
   </Instrument>
 </Spase>
diff --git a/Instrument/AMDA/Cluster-Salsa/PEACE.xml b/Instrument/AMDA/Cluster-Salsa/PEACE.xml
index d7c2cba..5d6dc18 100644
--- a/Instrument/AMDA/Cluster-Salsa/PEACE.xml
+++ b/Instrument/AMDA/Cluster-Salsa/PEACE.xml
@@ -6,21 +6,44 @@
     <ResourceHeader>
       <ResourceName>PEACE</ResourceName>
       <AlternateName>Plasma Electron and Current Experiment</AlternateName>
-      <ReleaseDate>2011-02-04T15:37:33Z</ReleaseDate>
-      <Description>The primary task of this instrument (PEACE: Plasma Electrons and Currents Experiment) is to obtain the velocity moments of the distribution function of electrons as frequently and as accurately as the spacecraft telemetry will allow. Detector counts are collected in energy, polar-angle, and azimuth-angle bins to form a three-dimensional matrix. Two sensors are used: LEEA (low-energy electron analyzer) and HEEA (high-energy electron analyzer). The energy coverage is from 0.67 eV to 30 KeV in 92 levels. The first 16 levels are equally spaced linearly up to 10.7 eV; the remainder are logarithmically spaced. Both sensors can use the full range, but the HEEA will normally operate over a higher energy range than the LEEA. The LEEA specializes in coverage of the energies from 0.7--10 eV, and has a geometric factor one fifth that of the HEAA. Both sensors consist of hemispherical electrostatic analyzers of the top-hat type and a detector in the form of an annular micro-channel plate with a position-sensitive readout. Each sensor covers the range 0--180 degrees with respect to the spin axis, and they are mounted opposite each other with a view perpendicular to the spin axis, thus covering the complete angular range in a half rotation of the spacecraft. The field of view perpendicular to the fan is 2 degrees for the LEEA and 5.6 degrees for the HEEA. Energy resolution (Delta-E)/E is 0.13 for LEEA and 0.16 for HEEA. There are four sweep modes, synchronized to the spin period (4 s), to vary the azimuthal angular resolution. The spin phasing can be made coincident with that of the CIS instrument, to ensure that the electron and ion moments will be measured simultaneously. On-board processing is used to calculate the moments of the distribution with an accuracy of 1% and to select suitable parts of the complete distribution for transmission. The normal science data format is based on one spin period, and consists of core data followed by other optional distributions as can be fit into the available telemetry for that spin. The core data (moments, spacecraft potential, and pitch angle distribution) are always transmitted (if the spin is nominal). The next distribution is transmitted if, before the end of the spin, all the previous data have been sent. Thus the next spin of data will be transmitted slightly late, but all of its core data will be transmitted before the following spin of data is started on. Eventually the transmission will catch up and be able to transmit the distribution after the core again, but only after some time. This applies at all telemetry rates. The instrument can adapt automatically to six different telemetry rates: a basic 1.52 Kbps rate (CIS priority); a normal 2.52 Kbps rate; an enhanced PEACE priority rate of 3.54 Kbps; and three burst mode rates, with a maximum of 15.98 Kbps. For more details of the Cluster mission, the spacecraft, and its instruments, see the report ``Cluster: mission, payload and supporting activities,'' March 1993, ESA SP-1159, and the included article ``PEACE: a Plasma Electron and Current Experiment,'' by A. D. Johnstone et al., from which this information was obtained.</Description>
+      <ReleaseDate>2016-11-04T15:37:46Z</ReleaseDate>
+      <Description>
+        The PEACE instrument consists of two sensors, HEEA (High Energy Electron Analyser) and LEEA (Low Energy Electron 
+        Analyser),  and  a  data  processing  unit,  the  DPU.  The  sensors  are  Top  Hat  electrostatic  analysers.  The  basic  measurement 
+        made by PEACE is the  number of counted electrons per accumulation time. The satellite spin period, Tspin
+        , is measured as  the time taken between two detections of the
+        Sun by the  spacecraft sun sensor (which is expected to be 4 seconds ±10%). 
+        Within  the  PEACE  DPU,  the  spin  period  is subdivided  into  1024  equal  parts,  of  duration  Tacc
+        ,  the PEACE accumulation time. The instrument measurement cycle 
+        is thus adjusted to match the spin period so that PEACE collects data from a  full 
+        4pi solid angle (i.e. provides all-sky coverage) during each and every spin. For a nominal 4 second spin, Tacc
+        ~ 3.9 msec.
+        In reality this is calculated from the duration of the previous spin
+        provided by the spacecraft housekeeping.
+      </Description>
+      <Acknowledgement>Principal Investigator: Andrew Fazakerley</Acknowledgement>
       <Contact>
         <PersonID>spase://SMWG/Person/Andrew.N.Fazakerley</PersonID>
         <Role>PrincipalInvestigator</Role>
       </Contact>
       <InformationURL>
+        <Name>ESA web page</Name>
+        <URL>http://sci.esa.int/jump.cfm?oid=33024</URL>
+        <Description>PEACE</Description>
+      </InformationURL>
+      <InformationURL>
         <Name>NSSDC's Master Catalog</Name>
-        <URL>http://nssdc.gsfc.nasa.gov/database/MasterCatalog?sc=2000-041B&amp;ex=5</URL>
+        <URL>http://nssdc.gsfc.nasa.gov/database/MasterCatalog?sc=2000-045A&amp;ex=5</URL>
         <Description>Information about the Plasma Electron and Current Experiment (PEACE) experiment on the Cluster 2/FM6 (Salsa) mission.</Description>
       </InformationURL>
       <PriorID>spase://SMWG/Instrument/Cluster2-Salsa/PEACE</PriorID>
     </ResourceHeader>
-    <InstrumentType>EnergeticParticleInstrument</InstrumentType>
-    <InvestigationName>Plasma Electron and Current Experiment (PEACE) on Cluster 2/FM6 (Salsa)</InvestigationName>
+    <InstrumentType>ElectrostaticAnalyser</InstrumentType>
+    <InvestigationName></InvestigationName>
+    <OperatingSpan>
+      <StartDate>2000-12-01T00:00:00</StartDate>
+      <Note>Start of full orbit coverage: 2002-06-01T00:00:00</Note>
+    </OperatingSpan>
     <ObservatoryID>spase://CDPP/Observatory/AMDA/Cluster-Salsa</ObservatoryID>
   </Instrument>
 </Spase>
diff --git a/Instrument/AMDA/Cluster-Samba/PEACE.xml b/Instrument/AMDA/Cluster-Samba/PEACE.xml
index 80201d6..9c98b58 100644
--- a/Instrument/AMDA/Cluster-Samba/PEACE.xml
+++ b/Instrument/AMDA/Cluster-Samba/PEACE.xml
@@ -6,21 +6,45 @@
     <ResourceHeader>
       <ResourceName>PEACE</ResourceName>
       <AlternateName>Plasma Electron and Current Experiment</AlternateName>
-      <ReleaseDate>2011-02-04T15:37:07Z</ReleaseDate>
-      <Description>The primary task of this instrument (PEACE: Plasma Electrons and Currents Experiment) is to obtain the velocity moments of the distribution function of electrons as frequently and as accurately as the spacecraft telemetry will allow. Detector counts are collected in energy, polar-angle, and azimuth-angle bins to form a three-dimensional matrix. Two sensors are used: LEEA (low-energy electron analyzer) and HEEA (high-energy electron analyzer). The energy coverage is from 0.67 eV to 30 KeV in 92 levels. The first 16 levels are equally spaced linearly up to 10.7 eV; the remainder are logarithmically spaced. Both sensors can use the full range, but the HEEA will normally operate over a higher energy range than the LEEA. The LEEA specializes in coverage of the energies from 0.7--10 eV, and has a geometric factor one fifth that of the HEAA. Both sensors consist of hemispherical electrostatic analyzers of the top-hat type and a detector in the form of an annular micro-channel plate with a position-sensitive readout. Each sensor covers the range 0--180 degrees with respect to the spin axis, and they are mounted opposite each other with a view perpendicular to the spin axis, thus covering the complete angular range in a half rotation of the spacecraft. The field of view perpendicular to the fan is 2 degrees for the LEEA and 5.6 degrees for the HEEA. Energy resolution (Delta-E)/E is 0.13 for LEEA and 0.16 for HEEA. There are four sweep modes, synchronized to the spin period (4 s), to vary the azimuthal angular resolution. The spin phasing can be made coincident with that of the CIS instrument, to ensure that the electron and ion moments will be measured simultaneously. On-board processing is used to calculate the moments of the distribution with an accuracy of 1% and to select suitable parts of the complete distribution for transmission. The normal science data format is based on one spin period, and consists of core data followed by other optional distributions as can be fit into the available telemetry for that spin. The core data (moments, spacecraft potential, and pitch angle distribution) are always transmitted (if the spin is nominal). The next distribution is transmitted if, before the end of the spin, all the previous data have been sent. Thus the next spin of data will be transmitted slightly late, but all of its core data will be transmitted before the following spin of data is started on. Eventually the transmission will catch up and be able to transmit the distribution after the core again, but only after some time. This applies at all telemetry rates. The instrument can adapt automatically to six different telemetry rates: a basic 1.52 Kbps rate (CIS priority); a normal 2.52 Kbps rate; an enhanced PEACE priority rate of 3.54 Kbps; and three burst mode rates, with a maximum of 15.98 Kbps. For more details of the Cluster mission, the spacecraft, and its instruments, see the report ``Cluster: mission, payload and supporting activities,'' March 1993, ESA SP-1159, and the included article ``PEACE: a Plasma Electron and Current Experiment,'' by A. D. Johnstone et al., from which this information was obtained.</Description>
+      <ReleaseDate>2016-11-04T15:37:46Z</ReleaseDate>
+      <Description>
+        The PEACE instrument consists of two sensors, HEEA (High Energy Electron Analyser) and LEEA (Low Energy Electron 
+        Analyser),  and  a  data  processing  unit,  the  DPU.  The  sensors  are  Top  Hat  electrostatic  analysers.  The  basic  measurement 
+        made by PEACE is the  number of counted electrons per accumulation time. The satellite spin period, Tspin
+        , is measured as  the time taken between two detections of the
+        Sun by the  spacecraft sun sensor (which is expected to be 4 seconds ±10%). 
+        Within  the  PEACE  DPU,  the  spin  period  is subdivided  into  1024  equal  parts,  of  duration  Tacc
+        ,  the PEACE accumulation time. The instrument measurement cycle 
+        is thus adjusted to match the spin period so that PEACE collects data from a  full 
+        4pi solid angle (i.e. provides all-sky coverage) during each and every spin. For a nominal 4 second spin, Tacc
+        ~ 3.9 msec.
+        In reality this is calculated from the duration of the previous spin
+        provided by the spacecraft housekeeping.
+      </Description>
+      <Acknowledgement>Principal Investigator: Andrew Fazakerley</Acknowledgement>
       <Contact>
         <PersonID>spase://SMWG/Person/Andrew.N.Fazakerley</PersonID>
         <Role>PrincipalInvestigator</Role>
       </Contact>
       <InformationURL>
+        <Name>ESA web page</Name>
+        <URL>http://sci.esa.int/jump.cfm?oid=33024</URL>
+        <Description>PEACE</Description>
+      </InformationURL>
+      <InformationURL>
         <Name>NSSDC's Master Catalog</Name>
-        <URL>http://nssdc.gsfc.nasa.gov/database/MasterCatalog?sc=2000-041A&amp;ex=5</URL>
+        <URL>http://nssdc.gsfc.nasa.gov/database/MasterCatalog?sc=2000-045A&amp;ex=5</URL>
         <Description>Information about the Plasma Electron and Current Experiment (PEACE) experiment on the Cluster 2/FM7 (Samba) mission.</Description>
       </InformationURL>
       <PriorID>spase://SMWG/Instrument/Cluster2-Samba/PEACE</PriorID>
     </ResourceHeader>
-    <InstrumentType>EnergeticParticleInstrument</InstrumentType>
-    <InvestigationName>Plasma Electron and Current Experiment (PEACE) on Cluster 2/FM7 (Samba)</InvestigationName>
+    <InstrumentType>ElectrostaticAnalyser</InstrumentType>
+    <InvestigationName></InvestigationName>
+    <OperatingSpan>
+      <StartDate>2000-12-01T00:00:00</StartDate>
+      <Note>Start of full orbit coverage: 2002-06-01T00:00:00</Note>
+      <Note>C3 spacecraft tilt by 40° during one month: 2008-05-01T00:00:00</Note>
+    </OperatingSpan>
     <ObservatoryID>spase://CDPP/Observatory/AMDA/Cluster-Samba</ObservatoryID>
   </Instrument>
 </Spase>
diff --git a/Instrument/AMDA/Cluster-Tango/PEACE.xml b/Instrument/AMDA/Cluster-Tango/PEACE.xml
index c4d72e0..a6b0ea2 100644
--- a/Instrument/AMDA/Cluster-Tango/PEACE.xml
+++ b/Instrument/AMDA/Cluster-Tango/PEACE.xml
@@ -6,21 +6,44 @@
     <ResourceHeader>
       <ResourceName>PEACE</ResourceName>
       <AlternateName>Plasma Electron and Current Experiment</AlternateName>
-      <ReleaseDate>2011-02-04T15:37:19Z</ReleaseDate>
-      <Description>The primary task of this instrument (PEACE: Plasma Electrons and Currents Experiment) is to obtain the velocity moments of the distribution function of electrons as frequently and as accurately as the spacecraft telemetry will allow. Detector counts are collected in energy, polar-angle, and azimuth-angle bins to form a three-dimensional matrix. Two sensors are used: LEEA (low-energy electron analyzer) and HEEA (high-energy electron analyzer). The energy coverage is from 0.67 eV to 30 KeV in 92 levels. The first 16 levels are equally spaced linearly up to 10.7 eV; the remainder are logarithmically spaced. Both sensors can use the full range, but the HEEA will normally operate over a higher energy range than the LEEA. The LEEA specializes in coverage of the energies from 0.7--10 eV, and has a geometric factor one fifth that of the HEAA. Both sensors consist of hemispherical electrostatic analyzers of the top-hat type and a detector in the form of an annular micro-channel plate with a position-sensitive readout. Each sensor covers the range 0--180 degrees with respect to the spin axis, and they are mounted opposite each other with a view perpendicular to the spin axis, thus covering the complete angular range in a half rotation of the spacecraft. The field of view perpendicular to the fan is 2 degrees for the LEEA and 5.6 degrees for the HEEA. Energy resolution (Delta-E)/E is 0.13 for LEEA and 0.16 for HEEA. There are four sweep modes, synchronized to the spin period (4 s), to vary the azimuthal angular resolution. The spin phasing can be made coincident with that of the CIS instrument, to ensure that the electron and ion moments will be measured simultaneously. On-board processing is used to calculate the moments of the distribution with an accuracy of 1% and to select suitable parts of the complete distribution for transmission. The normal science data format is based on one spin period, and consists of core data followed by other optional distributions as can be fit into the available telemetry for that spin. The core data (moments, spacecraft potential, and pitch angle distribution) are always transmitted (if the spin is nominal). The next distribution is transmitted if, before the end of the spin, all the previous data have been sent. Thus the next spin of data will be transmitted slightly late, but all of its core data will be transmitted before the following spin of data is started on. Eventually the transmission will catch up and be able to transmit the distribution after the core again, but only after some time. This applies at all telemetry rates. The instrument can adapt automatically to six different telemetry rates: a basic 1.52 Kbps rate (CIS priority); a normal 2.52 Kbps rate; an enhanced PEACE priority rate of 3.54 Kbps; and three burst mode rates, with a maximum of 15.98 Kbps. For more details of the Cluster mission, the spacecraft, and its instruments, see the report ``Cluster: mission, payload and supporting activities,'' March 1993, ESA SP-1159, and the included article ``PEACE: a Plasma Electron and Current Experiment,'' by A. D. Johnstone et al., from which this information was obtained.</Description>
+      <ReleaseDate>2016-11-04T15:37:46Z</ReleaseDate>
+      <Description>
+        The PEACE instrument consists of two sensors, HEEA (High Energy Electron Analyser) and LEEA (Low Energy Electron 
+        Analyser),  and  a  data  processing  unit,  the  DPU.  The  sensors  are  Top  Hat  electrostatic  analysers.  The  basic  measurement 
+        made by PEACE is the  number of counted electrons per accumulation time. The satellite spin period, Tspin
+        , is measured as  the time taken between two detections of the
+        Sun by the  spacecraft sun sensor (which is expected to be 4 seconds ±10%). 
+        Within  the  PEACE  DPU,  the  spin  period  is subdivided  into  1024  equal  parts,  of  duration  Tacc
+        ,  the PEACE accumulation time. The instrument measurement cycle 
+        is thus adjusted to match the spin period so that PEACE collects data from a  full 
+        4pi solid angle (i.e. provides all-sky coverage) during each and every spin. For a nominal 4 second spin, Tacc
+        ~ 3.9 msec.
+        In reality this is calculated from the duration of the previous spin
+        provided by the spacecraft housekeeping.
+      </Description>
+      <Acknowledgement>Principal Investigator: Andrew Fazakerley</Acknowledgement>
       <Contact>
         <PersonID>spase://SMWG/Person/Andrew.N.Fazakerley</PersonID>
         <Role>PrincipalInvestigator</Role>
       </Contact>
       <InformationURL>
+        <Name>ESA web page</Name>
+        <URL>http://sci.esa.int/jump.cfm?oid=33024</URL>
+        <Description>PEACE</Description>
+      </InformationURL>
+      <InformationURL>
         <Name>NSSDC's Master Catalog</Name>
-        <URL>http://nssdc.gsfc.nasa.gov/database/MasterCatalog?sc=2000-045B&amp;ex=5</URL>
+        <URL>http://nssdc.gsfc.nasa.gov/database/MasterCatalog?sc=2000-045A&amp;ex=5</URL>
         <Description>Information about the Plasma Electron and Current Experiment (PEACE) experiment on the Cluster 2/FM8 (Tango) mission.</Description>
       </InformationURL>
       <PriorID>spase://SMWG/Instrument/Cluster2-Tango/PEACE</PriorID>
     </ResourceHeader>
-    <InstrumentType>EnergeticParticleInstrument</InstrumentType>
-    <InvestigationName>Plasma Electron and Current Experiment (PEACE) on Cluster 2/FM8 (Tango)</InvestigationName>
+    <InstrumentType>ElectrostaticAnalyser</InstrumentType>
+    <InvestigationName></InvestigationName>
+    <OperatingSpan>
+      <StartDate>2000-12-01T00:00:00</StartDate>
+      <Note>Start of full orbit coverage: 2002-06-01T00:00:00</Note>
+    </OperatingSpan>
     <ObservatoryID>spase://CDPP/Observatory/AMDA/Cluster-Tango</ObservatoryID>
   </Instrument>
 </Spase>
diff --git a/NumericalData/AMDA/ACE/MFI/ace-mag-real.xml b/NumericalData/AMDA/ACE/MFI/ace-mag-real.xml
index eebac29..43baa9f 100644
--- a/NumericalData/AMDA/ACE/MFI/ace-mag-real.xml
+++ b/NumericalData/AMDA/ACE/MFI/ace-mag-real.xml
@@ -51,7 +51,7 @@
       <TemporalDescription>
          <TimeSpan>
              <StartDate>2014-01-06T00:00:00Z</StartDate>
-             <StopDate>2016-11-02T00:59:59Z</StopDate>
+             <StopDate>2016-11-03T00:59:59Z</StopDate>
          </TimeSpan>
          <Cadence>PT60S</Cadence>
       </TemporalDescription>
diff --git a/NumericalData/AMDA/ACE/SWEPAM/ace-swepam-real.xml b/NumericalData/AMDA/ACE/SWEPAM/ace-swepam-real.xml
index 83541f2..ca24937 100644
--- a/NumericalData/AMDA/ACE/SWEPAM/ace-swepam-real.xml
+++ b/NumericalData/AMDA/ACE/SWEPAM/ace-swepam-real.xml
@@ -44,7 +44,7 @@
    <TemporalDescription>
       <TimeSpan>
          <StartDate>2014-01-06T00:00:00Z</StartDate>
-         <StopDate>2016-11-02T00:59:59Z</StopDate>
+         <StopDate>2016-11-03T00:59:59Z</StopDate>
      </TimeSpan>
      <Cadence>PT60S</Cadence>
    </TemporalDescription>
--
libgit2 0.21.2