THE HIPPARCOS SOLAR SYSTEM OBJECTS ANNEXES D. Hestroffer
35
THE HIPPARCOS SOLAR SYSTEM OBJECTS ANNEXES
D. Hestro er
Astrophysics Division, ESTEC, NL-2200AG No ordwijk, The Netherlands
Bec-Borsenb erger 1997. The observations of plane- ABSTRACT
tary satellites relative to the background stars yield,
in an indirect manner, accurate p ositions of the grav-
Astrometric and photometric measurements of a
itating ma jor planet's centre of mass Morrison et al.
numb er of solar system ob jects were p erformed by the
1997; Fienga et al. 1997. Photometric observations
Hipparcos satellite in b oth the Hipparcos main mis-
of asteroids provides information ab out their rota-
sion and the Tycho exp eriment. The sp eci c asp ects
tional prop erties such as shap e and spin-vector orien-
of the Hipparcos observations and reduction pro cess
tation, and the scattering prop erties of their surface.
implemented for the solar system ob jects are pre-
Hence observations of such primordial ob jects yield
sented. Sp ecial attention is paid to the error budget
insight on their collisional evolution, and on the early
of the reduction which is accurate to the mas milli-
solar system.
arcsecond level for the Hipparcos main mission. The
contents of the Hipparcos Solar System Ob jects Cat-
The Hipparcos satellite successfully observed the so-
alogues is describ ed. Comparison b etween the results
lar system ob jects during its almost 4 years mission
derived from the two Consortia FAST and NDAC, as
duration. Hence it provides astrometric as well as
well as comparison with ground-based observations,
photometric information on these relatively bright
are given.
ob jects. The retained ob jects and the geometry of
the Hipparcos observations are brie y presented in
Section 2. The information gathered by the star
mapp er constitutes the Tycho Catalogue, while the
Key words: Astrometry, photometry, solar system.
Hipparcos Catalogue is derived from the observations
made through the main grid. The reduction of the
solar system ob jects observations follows the pro ce-
1. INTRODUCTION
dure retained for the stars on the rst stages, and
is adapted to these rapidly moving and eventually
resolved ob jects. The data are of di erent nature
Among the thousands of stars, the Hipparcos pro-
and precision and are presented separately in Sec-
gramme included a selection of solar system ob jects
tions 3 and 4. All astrometric p ositions are given in
ma jor planets, planetary satellites and asteroids.
the ICRS, and the transformation is presented in Sec-
The primary motivation is to provide highly accurate
tion 5. Comparison with ground-based observations
p ositions for the link of the dynamical reference sys-
and calculated places, and between the NDAC and
tem to the International Celestial Reference System
FAST p ositions, are given in Section 6.
ICRS, but also to enable dynamical and physical
studies of these ob jects. The value of astrometric
observations of asteroids, relatively to the reference
frame de ned by the stars, for the establishmentof
2. HIPPARCOS OBSERVATIONS
the dynamical reference frame, was rst suggested by
Dyson 1928. These ob jects were thought to con-
siderably enhance the results obtained from observa-
2.1. Observing Programme
tions of the Sun or ma jor planets. Nonetheless, this
metho d encountered some limitations; hence such ob-
Initially two satellites Europa and Titan and 63
servations of minor planets enter for instance in the
asteroids were retained in the Hipparcos main mis-
solution derived by Fricke 1982 for the FK5 with
sion programme. Positions of the solar system ob-
a relatively mo dest weight. Hipparcos should dra-
jects were entered in the Input Catalogue by means
matically improve the situation e.g. Hestro er et al.
of their ephemerides Bec-Borsenb erger 1985. Since
1995; Bec-Borsenb erger et al. 1995, and yield a link
the p ositions had to b e known a priori with a preci-
between the dynamical system and the ICRS with a
sion b etter than 1 arcsec, a ground-based campaign of
precision of the same order of magnitude as the b est
observations of these asteroids was started in 1983 in
result obtained so far Folkner et al. 1994.
order to improve the accuracy of their ephemerides.
High precision measures of the p ositions of asteroids
The numb er of retained asteroids was reduced to 48
enables to improve their ephemerides but also in par-
after consideration of the numb er of their predicted
ticular cases of very close encounters to determine the
transits during the scheduled nominal mission dura-
mass of some of them e.g. Viateau 1997; Bange &
tion. The Saturnian satellite S8 Iap etus was added
36
to the observation programme during the mission. for Venus, Mars, Jupiter and Saturn. Next, the ob-
A priori ephemerides of the 48 Hipparcos asteroids, jects brighter than V 10 and with sucientnum-
the four Galilean satellites, Titan, Venus and planets b er of observations were retained; the list is given in
Mars through Neptune were also calculated as part of Table 1. When available, the photometry is provided
the Tycho Input Catalogue of 3 million stars. Never- in the Tycho B and V passbands which, although
T T
theless, not all of these solar system ob jects were re- not identical, are close to the Johnson B and V . Over
tained for the Catalogue output see Section 3; their the range 0:2 < B V < 1:8, the following lin-
T
inclusion was necessary for technical reasons Bastian ear formulae yield transformations b etween the two
&Wagner 1997. photometric systems accurate to 0.05 mag:
V V = 0:09 B V
T J T
2.2. A Scanning Satellite
B V = 0:85 B V
J T
Since the Hipparcos satellite was scanning the whole
sky in a regular manner, no p ointing to a sp eci c ob-
z
ject was p ossible; but an observation o ccurred dur-
Moreover the
ing its transit across the eld of view. Star motion
spin axis of the satellite was precessing with a con-
stant angle of 43 around the direction towards the
45 o
enabling a complete and optimal coverage of
Sun, w
the celestial sphere. On the other hand, solar sys-
tem ob jects are gravitating around the Sun in a band
20'
near the ecliptic, thus observations of these ob jects
are spread around the quadratures see Figure 1, i.e.
when the solar phase angle is maximal. Also the total
0"91 0"91 5"63
numb er of observations is varied b etween the di er-
Figure2. Schematic view of the star mapper slits system.
ent observed ob jects from roughly 15 to 125 tran-
All slits have the same width in the direction of the w
sits. The same remark applies for the distribution
axis. The inclined and vertical slits are spaced, in the
of these transits in time or along the planet's tra jec-
tory. The Hipparcos and Tycho observations are of
direction of a star's motion, with distance ratio 2:3:1 of
course almost simultaneous; a transit across the star
the step s = 5 :63 arcsec. The ` ducial lines', which can
mapp er o ccurs a few seconds b efore the transit across
be thought as the centres of gravity of the four slits in each
the main grid.
group, are shown as dashed lines.
Quadrature
Table 1. Solar system objects of the Tycho Catalogue. (2) (3)
asteroid (1)
Name Photometry Astrometry Rotation
axis Minor planets:
p p
1 Ceres p
(1) p
2 Pallas
p p esta
86° 4 V
p p
6 Heb e
p p
Sun 7 Iris Satellite Satellites:
(2) p
J I I I{Ganymede {
p
J IV{Callisto {
p p S VI{Titan
(3)
Ma jor planets:
p
Uranus {
p
Neptune {
Figure 1. Schematic view of the Hipparcos satel lite's
scanning law. The observations of solar system objects
are made around the quadratures.
The magnitudes in the twochannels are derived, in
the same way as for the stars, from the amplitude
3. TYCHO
of the convolved signal and are calculated by a sim-
pli ed calibration pro cedure. The magnitude pro-
vided for each transit corresp onds to the mean of the
The data gathered by the star mapp er constitute the
measure for each slits group crossing. No magnitude
Tycho Catalogue. Aschematic view of the grid sys-
is provided for ob jects larger in apparent size than
tem is given in Figure 2. The Tycho observations are
the width of the slits 0.91 arcsec. For ob jects that
not adapted to ob jects larger in apparent size than
were not substantially smaller than the slit's width,
the smallest separation b etween two slits 5.63 arc-
systematic errors may o ccur. Finally, no standard er-
sec. At least for this reason no data can b e provided
rors are provided for the estimation of the B and V
T T
37
magnitudes; they are of the order of 0.1 mag for an ; , the standard errors ; and the corre-
ob ject of magnitude V 8 and 0.35 mag for V 10.
lation between the two co ordinates . To enable
future systematic correction of the data, esp ecially
Since the transits across each slits group yield in-
for the large ma jor planets, the p osition angle ,
formation in two directions, one can derive a con-
the inclined-slit ag signz , and the standard errors
ventional two-dimensional p osition on the celestial
; are provided as additional data. All p ositions
1 2
sphere for each transit. The displacement of the so-
are referred to the ICRS system see Section 5. It is
lar system ob ject b etween the crossing of the ducial
stressed that phase, shap e or alb edo corrections are
lines of the slit groups in a time interval up to ab out
not taken into account. The p osition corresp onds to
10 s is known with sucient accuracy to enable such
the photo centre for the smallest ob jects. For Uranus,
a construction. The primary astrometric information
Neptune and to a lesser extent the twoJovian satel-
is the time when an ob ject crosses the ducial line as
lites, whose angular diameters are larger than the
derived in the detection and estimation pro cess. The
slit width, the p osition on the surface of the body
di erence b etween the observed and predicted cross-
dep ends highly on its alb edo distribution and the
ing time for each slit group is converted into an along-
scanning geometry. More accurate correction to the
scan residual on p osition. Next the two along-scan
centre of gure can b e applied by a simulation of the
residuals u ; u are transformed into residuals
1 2
Tycho photon counts and convolution with the slit
in the two orthogonal directions w and z asso ciated to
resp onse. A general description of the pro cedure to
the fo cal plane of the telescop e. This transformation
follow is given in the Hipparcos Catalogue Hg &
P dep ends on the sign of the z co ordinate, whether
Makarov 1997.
the transit o ccurs in the upp er part sgnz = +1
or the lower part sgnz = 1 of the inclined slits.
The orientation of the w; z frame on the celestial
4. HIPPARCOS
sphere is given by the p osition angle . The observed
p osition, at the|arbitrarily chosen|reference ep o ch
t , is thus derived from an a priori calculated p osi-
2
In contrast to the star mapp er, the main grid is
tion close to the true p osition and the along-scan
made of `vertical' slits, and hence only provides a
residuals by:
one-dimensional p osition, i.e. the observed p osition
lo cus in the direction p erp endicular to the slits. As-
u
2 1
= R P 1
trometry is provided for ob jects brighter than V 13
u
2 2
and smaller in apparent size than 1 arcsec, i.e. 48
asteroids, the planetary satellites J2 Europa, S6 Ti-
where = cos , and where:
tan and S8 Iap etus unfortunately only a very few
observations are available for Iap etus.
sin cos
R =
cos sin
The primary astrometric and photometric informa-
tion is obtained from the Fourier expansion of the
0 1
mo dulated signal:
P =
signz signz
S t = I [1 + M cos!t + '
The second-order terms arising from the transfor-
mation between the tangent plane and the celestial
+ N cos2!t +2] 2
sphere are neglected. Intro ducing the diagonal ma-
trix of the standard error of the measurements:
where ! is the fundamental angular frequency. This
reduces for a p oint-like source to:
0
1
=
0
2
S t = I [1 + M cos!t + '
o o
the variance matrix of the derived co ordinates is
+ N cos2!t +2' ] 3
o o
given by:
0 1
where M ;N are calibrated mo dulation co ecients,
o o
2
and the mo dulation phases are indep endent of the
2 0 0
@ A
= R P P R
harmonic rank ' = = ' . The astrometry is
o
2
given at this stage by an abscissa v as derived from
the mo dulation phases '; within FAST, and the
This matrix is no longer diagonal, re ecting the fact
phase ', of the rst harmonic only, within NDAC.
that|dep ending on the p osition angle and the ra-
For a p oint-like or relatively small source typically
<
tio = |the principal axis of the asso ciated error
with a diameter 0:05 arcsec, the FAST and
1 2
ellipse do es not coincide with the N,E directions to-
NDAC abscissae have the same exp ectancy since the
ward the northern celestial p ole and the east. The
calibrated phases ' and are almost equal. For
along-scan standard errors are derived from an error
a larger extended source, the di erence b etween the
mo del adequate for stellar images and do not corre-
FAST and NDAC abscissa dep ends on the physical
sp ond to a Gaussian noise. Moreover, the signals for
prop erties of the minor planet or planetary satellite
planets are broader and more at at the top than the
such as apparent diameter, solar phase angle, alb edo
signals of p oint-like sources. Thus the derived quan-
distribution over the visible surface and scanning ge-
2 2
ometry.
tities and should preferably be regarded as
indicators of the quality of a single measure.
In contrast to the stars, the FAST and NDAC so-
For each transit, the astrometric observation is de- lutions have not b een merged into a single p osition.
ned by the reference epoch t , the co ordinates The FAST reduction pro cedure is not adapted to the 2
38
observations of the largest ob jects J2 Europa and the apparent magnitude Hp and Hp are derived
dc ac
S6 Titan, thus only the NDAC p ositions are provided. from the co ecients I; IM; IN . The apparent mag-
For smaller ob jects, b oth pro cedures are valid; but as nitude Hp is directly given by the mean intensity
dc
noted b efore, the FAST and NDAC p ositions lo ci do I corrected for background noise. The second esti-
not strictly sp eaking corresp ond to the same p oint mator Hp is derived from the amplitude IM; IN
ac
on the surface of the ob ject. Hence, in order to avoid of the mo dulation. It is stressed that the Hp esti-
ac
intro ducing additional errors, no merging of the data mator, given as additional data, is of lower precision
was p erformed. Nevertheless, for the smallest b o dies and biased. Wehave, in a rst approximation, for a
relatively to the grid step, b oth FAST and NDAC spherical ob ject of apparent diameter :
lo ci corresp ond as a rst approximation to the p osi-
2 4
tion of the photo centre Hestro er & Mignard 1997.
Hp Hp a + o +o
ac dc
The displacement on the sky of an asteroid or a plan-
where a > 0 is a scalar and is the solar phase
etary satellite during the 17 seconds it takes to
angle. The transformation from the Hp system to
cross the main grid, can b e calculated with sucient
standard magnitudes are given by Mignard et al.
accuracy to enable the construction of a normal p o-
1997. The Hp and V bands have more or less
J
sition lo cus for each transit. A linear regression is
the same e ectivewavelength, they can b e related in
p erformed over the transit in order to determine the
a go o d approximation for solar system ob jects with
< <
average o set between the calculated and observed