20
XMM-Newton | ESA/ESOC | HSO-OAX | Page 1 CAL/OPS meetings M. Kirsch ESA/ESOC with input from the XMM FCT

CAL/OPS meetings · 2012. 3. 8. · 2 new modes (TCM4W, IPS4W)-Slight modification on AMD -TBD: check ESAM and FDIR • S/W-The average processor load is estimated to increase by

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Page 1: CAL/OPS meetings · 2012. 3. 8. · 2 new modes (TCM4W, IPS4W)-Slight modification on AMD -TBD: check ESAM and FDIR • S/W-The average processor load is estimated to increase by

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1

CAL/OPS m

eetings

M. Kirsch ESA/ESOC

with input from the XMM FCT

Page 2: CAL/OPS meetings · 2012. 3. 8. · 2 new modes (TCM4W, IPS4W)-Slight modification on AMD -TBD: check ESAM and FDIR • S/W-The average processor load is estimated to increase by

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2

menu

�sp

ace

cra

ft s

tatu

s &

mis

sio

n p

erf

orm

an

ce

�sp

ecia

l e

ve

nts

�o

utl

oo

k

Page 3: CAL/OPS meetings · 2012. 3. 8. · 2 new modes (TCM4W, IPS4W)-Slight modification on AMD -TBD: check ESAM and FDIR • S/W-The average processor load is estimated to increase by

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3

solar arrays

�p

ow

er

ge

ne

rati

on

ca

pa

bil

itie

s a

re n

orm

al

�n

o s

ign

of

un

ex

pe

cte

d d

eg

rad

ati

on

vis

ible A

ctua

l

Page 4: CAL/OPS meetings · 2012. 3. 8. · 2 new modes (TCM4W, IPS4W)-Slight modification on AMD -TBD: check ESAM and FDIR • S/W-The average processor load is estimated to increase by

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4

fuel

Rem

ain

ing

fu

el65

. [kg

]

Co

nsu

mp

tio

n la

st

12 m

on

th6.

2 [k

g]

aver

age

fuel

co

nsu

mp

tio

n

(sin

ce 2

003-

03-0

1)

0.48

[k

g/m

onth

]

resi

du

al li

feti

me

in

mo

nth

97 [-

]

extr

apo

late

d m

ilag

eF

eb.

2020

Page 5: CAL/OPS meetings · 2012. 3. 8. · 2 new modes (TCM4W, IPS4W)-Slight modification on AMD -TBD: check ESAM and FDIR • S/W-The average processor load is estimated to increase by

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5

LCL statistics

2012

:•0

2-01

-201

2: H

LCL

4.2A

trip

off

(pow

ers

2 he

ater

s of

the

mai

n br

anch

oft

he E

PIC

an

d R

GS

ele

ctro

nics

.)•2

012-

01-2

5: H

LCL

ST

A P

AN

B tr

ip o

ff (p

ower

s re

dund

ant I

MU

/RW

hea

ters

)

Page 6: CAL/OPS meetings · 2012. 3. 8. · 2 new modes (TCM4W, IPS4W)-Slight modification on AMD -TBD: check ESAM and FDIR • S/W-The average processor load is estimated to increase by

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6

spacecraft/mission status

Money

Fu

nd

ed

un

til

ne

xt

ex

ten

sio

n r

eq

ue

st

En

d 2

01

2/1

4in

20

12�

20

16

Fuel

rem

ain

ing

Use

pe

r y

ea

r

Mil

ea

ge

le

ft

65

kg

6 k

g

�2

02

0

Solar array power

Ma

xim

um

re

qu

ire

d

Cu

rre

nt

ma

rgin

Ma

rgin

en

d o

f 2

01

8

13

50

W

54

5 W

35

0 W

Battery

Acco

rdin

g t

o U

HB

15

+ y

Gyros/(IMUs)

Usa

ge

< 2

0 %

Reaction wheels

Usa

ge

< 4

4 %

RF switches

Transponder switches

Usa

ge

Stu

ck

at

on

e p

osit

ion

Ba

ck

up

no

t u

se

d

inste

ad

tra

nsp

on

de

rs a

re s

wit

ch

ed

TX

A L

CL

sw

itch

es

58

4

TX

B L

CL

sw

itch

es

59

5(Q

ua

lifi

ed

to

25

00

0)

Page 7: CAL/OPS meetings · 2012. 3. 8. · 2 new modes (TCM4W, IPS4W)-Slight modification on AMD -TBD: check ESAM and FDIR • S/W-The average processor load is estimated to increase by

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7

mission performance

Page 8: CAL/OPS meetings · 2012. 3. 8. · 2 new modes (TCM4W, IPS4W)-Slight modification on AMD -TBD: check ESAM and FDIR • S/W-The average processor load is estimated to increase by

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8

eclipse winter/spring 2011/2

�1

5/1

2-1

0/0

1

�m

ax

. d

isch

arg

e d

ura

tio

n:

0h

55

m5

5s

�M

ax

. D

ep

th o

f D

isch

arg

e:

17

.2 %

(1

00

%=

35

Ah

)

�A

uto

ma

ted

TT

ge

ne

rati

on

no

w f

ull

y o

pe

rati

on

al

Page 9: CAL/OPS meetings · 2012. 3. 8. · 2 new modes (TCM4W, IPS4W)-Slight modification on AMD -TBD: check ESAM and FDIR • S/W-The average processor load is estimated to increase by

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9

special events

�Collision avoidance i

n p

lace

(N

ov

em

be

r 2

01

1 –

Ma

rch

20

12

)

�R

ea

cti

on

wh

ee

l cage instability

: •

XM

M_

SC

-72

, 2

01

1-0

8-1

6,

Re

acti

on

Wh

ee

l 1

un

ex

pe

cte

d i

ncre

ase

in

to

rqu

e a

nd

cu

rre

nt

du

rin

g s

tab

le p

oin

tin

g

•S

wit

ch

of

rea

cti

on

wh

ee

l co

nfi

gu

rati

on

fro

m 1

-2-3

to

2-3

-4 i

n D

ece

mb

er

20

11

�4WD project

•W

he

el4

teste

d u

p t

o 3

75

0 r

pm

in

Ju

ly

�MCS m

igration

�Fuel migration

Page 10: CAL/OPS meetings · 2012. 3. 8. · 2 new modes (TCM4W, IPS4W)-Slight modification on AMD -TBD: check ESAM and FDIR • S/W-The average processor load is estimated to increase by

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10

collision avoidance

�X

MM

orb

it c

rossin

g G

EO

fo

r a

pe

rio

d o

f ~

5 m

on

th

�C

on

jun

cti

on

mo

nit

ori

ng

in

pla

ce

an

d p

roce

du

re f

or

co

llis

ion

av

oid

an

ce

ma

ne

uv

er

�D

ete

cte

d c

on

jun

cti

on

s (

Scre

en

ing

Vo

lum

e:

30

0k

m x

30

0k

m x

30

0k

m):

9

�N

o n

ee

d f

or

ma

ne

uv

er

so

fa

r (b

elo

w 2

0 k

m)

�O

bje

cts

: R

ock

et

bo

die

s (

3),

Ro

ck

et

bo

dy

de

b.

(3),

Sp

ace

cra

ft (

3)

Miss distance [km]

Page 11: CAL/OPS meetings · 2012. 3. 8. · 2 new modes (TCM4W, IPS4W)-Slight modification on AMD -TBD: check ESAM and FDIR • S/W-The average processor load is estimated to increase by

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11

cage instability: symptoms �

RW

1 c

om

ma

nd

ed

to

rqu

e a

nd

R

WD

E1

cu

rre

nt

so

me

tim

es d

uri

ng

sta

ble

po

inti

ng

su

ffe

rs a

ju

mp

�T

he

re

aso

n f

or

the

se

ju

mp

s i

s

mo

st

pro

ba

bly

a s

ud

de

n i

ncre

me

nt

of

the

be

ari

ng

fri

cti

on

le

ve

l.

�W

ell k

no

wn

ph

en

om

en

a w

ith

b

ea

rin

gs r

un

nin

g i

n m

arg

ina

lly

lu

bri

ca

ted

re

gim

es

�C

ha

oti

c v

ibra

tio

n o

f ca

ge

�C

au

se

d b

y t

oo

mu

ch

or

too

lit

tle

o

il

(la

te i

n t

he

mis

sio

n c

an

on

ly

be

du

e t

o r

ed

ucti

on

in

oil q

ua

nti

ty)

�V

ibra

tio

n c

au

se

s i

ncre

ase

d

fric

tio

n,

ca

use

s b

ea

rin

g t

o r

un

h

ott

er,

oil g

ets

th

inn

er

an

d g

ets

e

jecte

d f

rom

be

ari

ng

as m

icro

d

rop

lets

, o

il r

un

s h

ott

er,

oil s

tart

s

to d

eg

rad

e,

lig

hte

r fa

ts b

oil o

ff,

oil

run

s h

ott

er,

oil d

eg

rad

es f

urt

he

r,

oil r

un

s h

ott

er,

mo

re c

om

ple

x f

ats

b

oil o

ff,

be

ari

ng

ru

ns h

ott

er,

b

ea

rin

g f

ail

s

wheel 1 wheel 2

wheel 3

Tim

e [DOY 2010]

Torque [Nm]

310 331

Page 12: CAL/OPS meetings · 2012. 3. 8. · 2 new modes (TCM4W, IPS4W)-Slight modification on AMD -TBD: check ESAM and FDIR • S/W-The average processor load is estimated to increase by

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cage instability: analysis

�S

cre

en

da

ta f

or

no

n s

lew

an

d n

on

RW

B t

ime

s

�P

rod

uce

mo

nth

ly h

isto

gra

ms o

f co

mm

an

de

d t

orq

ue

�F

irst

pe

ak

sh

ow

s n

om

ina

l to

rqu

e d

istr

ibu

tio

n

�If

th

ere

is s

eco

nd

pe

ak

, th

is s

ho

ws c

ag

e i

nsta

bilit

y

�H

eig

ht/

inte

gra

l o

f se

co

nd

pe

ak

giv

es i

nd

ica

tio

n o

f a

mo

un

t o

f ca

gin

g

�D

iffe

ren

ce

of

pe

ak

po

sit

ion

be

twe

en

1st

an

d 2

nd

pe

ak

giv

es s

tre

ng

th o

f ca

gin

g

no cage instability

2006/09

cage instability RW1

2010/11

Page 13: CAL/OPS meetings · 2012. 3. 8. · 2 new modes (TCM4W, IPS4W)-Slight modification on AMD -TBD: check ESAM and FDIR • S/W-The average processor load is estimated to increase by

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cage instability analysis -

evolution

�a

na

lysis

of

his

tog

ram

plo

ts f

or

ea

ch

mo

nth

fro

m 2

00

5 u

nti

l n

ow

�cle

ar

on

-se

t o

f ca

ge

in

sta

bilit

y

in 2

00

8

�e

vo

luti

on

ov

er

the

la

st

2 y

ea

rs

sh

ow

s n

o s

ign

ific

an

t fu

rth

er

de

gra

da

tio

n

peakmax peak position

no caging peak

caging peak

caging peak

no caging peak

wheel1

wheel2

wheel3

Page 14: CAL/OPS meetings · 2012. 3. 8. · 2 new modes (TCM4W, IPS4W)-Slight modification on AMD -TBD: check ESAM and FDIR • S/W-The average processor load is estimated to increase by

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cage instability analysis –

butterfly plots

�P

lott

ing

wh

ee

l sp

ee

d v

ers

us

torq

ue

in

dic

ate

s i

f th

e c

ag

e i

nsta

bilit

y

is p

rese

nt

for

all

wh

ee

l sp

ee

ds

�F

or

hig

he

r sp

ee

ds

the

fa

cto

r in

to

rqu

e

incre

ase

du

rin

g t

he

ca

gin

g s

tate

do

es

fla

tte

n o

ff

Page 15: CAL/OPS meetings · 2012. 3. 8. · 2 new modes (TCM4W, IPS4W)-Slight modification on AMD -TBD: check ESAM and FDIR • S/W-The average processor load is estimated to increase by

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cage instability: actions taken

�A

SU

re

co

mm

en

de

d t

o g

o A

SA

P f

rom

wh

ee

l 1

-2-3

to

2-3

-4 c

on

tro

l

�A

fte

r te

sti

ng

on

th

e s

imu

lato

r w

he

el

1 h

as b

ee

n s

wit

ch

ed

of

an

d w

he

el

4 h

as b

ee

n

pu

t in

to c

on

tro

l

•F

/D c

on

fig

ura

tio

n c

on

tro

l is

su

e i

n c

om

bin

ati

on

wit

h F

/D d

esig

n i

ssu

e a

nd

TO

O r

eq

ue

st

ca

use

d a

n E

SA

M

en

try

so

me

da

ys l

ate

r

�W

he

el

1 i

s n

ow

wa

itin

g f

or

“re

-lu

bri

ca

tio

n”:

ea

ch

re

acti

on

wh

ee

l h

as a

n o

il

rese

rvo

ir,

tha

t a

llo

ws i

nje

cti

ng

oil i

n t

he

be

ari

ng

. T

his

sh

ou

ldcu

re t

he

ca

ge

in

sta

bilit

y

�C

urr

en

tly

Astr

ium

/Bra

dfo

rd i

n c

om

bin

ati

on

wit

h E

SO

C a

re

wo

rkin

g o

n a

pro

ce

du

re t

o p

erf

orm

th

is r

e-l

ub

rica

tio

n

Page 16: CAL/OPS meetings · 2012. 3. 8. · 2 new modes (TCM4W, IPS4W)-Slight modification on AMD -TBD: check ESAM and FDIR • S/W-The average processor load is estimated to increase by

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cage instability m

onitoring

�C

om

pa

rin

g t

he

pre

dic

ted

to

rqu

e

as a

fu

ncti

on

of

wh

ee

l sp

ee

d

wit

h t

he

actu

al

sp

ee

d o

ve

r ti

me

in

dic

ate

s w

he

n a

wh

ee

l is

in

ca

gin

g s

tag

e

�T

his

me

tho

d c

an

be

use

d n

ea

r re

al

tim

e

�W

eig

hti

ng

ca

ge

sta

tes w

ith

1

an

d o

ne

ca

ge

sta

ge

s w

ith

0

giv

es a

s w

ell t

he

ca

ge

fra

cti

on

in

a c

ert

ain

tim

e i

nte

rva

l

�T

his

me

tho

d i

s b

ee

n

imp

lem

en

ted

to

mo

nit

or

�D

eri

ve

d p

ara

me

ter

imp

lem

en

ted

on

MC

Ss

Page 17: CAL/OPS meetings · 2012. 3. 8. · 2 new modes (TCM4W, IPS4W)-Slight modification on AMD -TBD: check ESAM and FDIR • S/W-The average processor load is estimated to increase by

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fuel saving options

�4WD

: p

ote

nti

al

for

50

% o

f fu

el

sa

vin

g a

cco

rdin

g t

o F

/D e

sti

ma

tes

•F

ea

sib

ilit

y p

ha

se

1 h

as b

ee

n k

ick

ed

off

Se

pte

mb

er

20

11

wit

h A

str

ium

•A

lgo

rith

ms:

-2

ne

w m

od

es (

TC

M4

W,

IPS

4W

)

-S

lig

ht

mo

dif

ica

tio

n o

n A

MD

-T

BD

: ch

eck

ES

AM

an

d F

DIR

•S

/W -T

he

av

era

ge

pro

ce

sso

r lo

ad

is e

sti

ma

ted

to

in

cre

ase

by

< 1

%

-F

rom

a R

AM

me

mo

ry p

oin

t o

f v

iew

, a

bo

ut

~ 2

30

0 w

ord

s w

ill

be

re

qu

ire

d b

y t

he

n

ew

(8

00

0 w

ord

s s

till

av

ail

ab

le)

•C

ost

an

d s

ch

ed

ule

fo

r P

ha

se

2 (

imp

lem

en

tati

on

) w

ill

be

av

ail

ab

leb

y m

id A

pri

l

•D

ecis

ion

at

ME

OR

28

/06

�Reduction of wheel speed lim

its a

rou

nd

0 f

rom

20

0 r

pm

to

65

rp

m

�Flexible Perigee attitude

: d

ela

ye

d u

nti

l e

nd

of

co

llis

ion

mo

nit

ori

ng

, sin

ce

fix

ed

att

itu

de

is

req

uir

ed

Page 18: CAL/OPS meetings · 2012. 3. 8. · 2 new modes (TCM4W, IPS4W)-Slight modification on AMD -TBD: check ESAM and FDIR • S/W-The average processor load is estimated to increase by

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MCS m

igration

�M

issio

n C

on

tro

l S

yste

m H

/W h

as r

ea

ch

ed

its

en

d

of

life

su

pp

ort

�M

igra

tio

n p

roce

ss h

as b

ee

n s

tart

ed

•M

igra

tio

n t

o S

ola

ris 1

0 u

sin

g H

/P T

4 s

erv

er

•V

irtu

aliza

tio

n o

f C

lie

nts

an

d S

erv

ers

•M

igra

tio

n i

n p

ara

lle

l w

ith

IN

TE

GR

AL

•E

nd

of

pro

ce

ss i

n 2

01

3

•W

ill

mig

rate

as w

ell t

he

Ba

ck

Up

sy

ste

m a

t R

ed

u w

hile

m

ov

ing

it

to E

SA

C/C

eb

rero

s (

TB

D)

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XM

M-N

ew

ton

|E

SA

/ES

OC

| H

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-OA

X |

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19

fuel migration

�D

esig

n o

f T

an

k s

yste

m o

f X

MM

re

qu

ire

s f

ue

l m

igra

tio

n f

rom

a

ux

ilia

ry t

an

ks t

o m

ain

ta

nk

at

ne

ar

de

ple

tio

n s

tatu

s (

38

kg

le

ft)

�F

ue

l m

igra

tio

n w

ill

be

p

erf

orm

ed

by

te

mp

era

ture

d

elt

a b

etw

ee

n m

ain

ta

nk

an

d

au

x t

an

ks (

De

lta

T =

8-1

1 K

)

�F

irst

mig

rati

on

pro

ce

ss p

lan

ne

d

for

20

15

(3

WD

)

�M

igra

tio

n p

roce

ss n

ee

ds t

o b

e

rep

ea

ted

aft

er

usa

ge

of

8 k

g (

1

pe

r y

ea

r 4

WD

, ½

ye

ar

wit

h

3W

D)

Tank1

Tank2

Tank3

Tank4

2+2+2+2

Page 20: CAL/OPS meetings · 2012. 3. 8. · 2 new modes (TCM4W, IPS4W)-Slight modification on AMD -TBD: check ESAM and FDIR • S/W-The average processor load is estimated to increase by

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|E

SA

/ES

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20

outlook

�Astrium

final presentation for XMM 4WD 17/04

�UG m

eeting 19/04

�Mission Extension Operations Review 28/06

�MCS m

igration with finalization early 2013

�Wheel-1 re-lubrication in Summer

�Fuel Migration “dry-run”☺ ☺☺☺in autumn