jated 6x6
lon points
dard devi-
nd Z and
ted. The
erted nor-
lue of the
lerived by
the check
f the the-
eck points
al and the
stochastic
show that
id Z were
the check
)y system-
een image
state vec-
to along-
of the six
priori val-
1arily due
from the
ld not be
on from a
e synchro-
OK
orbit and
ry is pre-
2/WAOSS
time orbit
d into the
to a com-
The pro-
n of orbit
-versa, en-
the orbit
f scientific
The new concept will be routinely used for the forthcoming
MOMS-2P/PRIRODA mission aboard the Russian space
station MIR, scheduled for spring 1996. Within 18 months
MOMS-2P (MOMS-02, adapted to the PRIRODA envi-
ronment) will collect imagery from about 400 km orbital
height with a ground resolution of 6 m and 18 m respec-
tively. The dedicated MOMSNAV navigation package,
consisting of high precision GPS and INS ensures precise
orbit and attitude data, synchronized with the MOMS-2P
imagery by 0.1 msec. Since MOMS-2P/PRIRODA images
will enable a regional covering, a simultaneous block ad-
justment of several overlapping strips from different orbit
arcs which provides highly accurate results will be possible.
Another attractive application of the integrated concept is
based on 79 images of Ida and its satellite Dactyl obtained
by a CCD frame camera during the 2"? Galileo asteroid
flyby in August 1993. These images combined with orbit
and attitude data and orbital constraints provide a novel
opportunity to extract the physical parameters of Ida and
Dactyl, ie. size, shape and motion of the two objects, as
well as possibly also mass and density of Ida.
6 ACKNOWLEDGEMENTS
I would like to thank Eberhard Gill and Oliver Mon-
tenbruck at the GSOC/DLR for their great support. The
work presented in this paper is funded by grant 50 QM 9205
of the German Space Agency (DARA).
7 REFERENCES
Albertz J., Scholten F., Ebner H., Heipke C., Neukum G.
(1993): Two Camera Experiments on the Mars94/96
Missions; GIS 6(4), 11-16.
Baltsavias E. (1995): Private Communication.
Braun C.v., Reigber C. (1994): Space shuttle orbit deter-
mination using empirical force modelling of attitude ma-
neuvers for the German MOMS-02/D2 mission; Flight
Mechanics and Estimation Theory Symposium, God-
dard Space Flight Center, May 17-19, Greenbelt.
Case J.B. (1961): The Utilization of Constraints in Ana-
lytical Photogrammetry; Photogrammetric Engineering
25(5), 766-788.
Davies M.E., Abalakin V.K., Brahic A., Bursa M., Chovitz
B.H., Lieske .J.H. “Seidelmann PK... Sinclair, A. 1.
Tjuflin Y.S. (1992): Report of the IAU/IAG/COSPAR
Working Group on Cartographic Coordinates and Ro-
tational Elements of the Planets and Satellites: 1991;
Celestial Mechanics 53, 377—397.
Davis R., Riding T. (1970): The Rigorous and Simulta-
neous Adjustment of Lunar Orbiter Photography Con-
sidering Orbital Constraints; RADC-TR-70-274, Rome
Air Development Center, National Technical Informa-
tion Center, Springfield, Virginia.
Ebner H., Kornus W., Ohlhof T. (1994a): A simulation
study on point determination for the MOMS-02/D2
Space Project using an extended functional model; GIS
7(1), 11-16.
Ebner H., Ohlhof T, Tang L. (1994b): Eine Studie zur
Bildzuordnung und Punktbestimmung im Rahmen der
Mars94-Mission; Zeitschrift für Photogrammetrie und
Fernerkundung 62(2), 57-71.
International Archives of Photogrammetry and Remote Sensing. Vol. XXXI, Part B3. Vienna 1996
Eckardt A. (1995): The performance of the new Wide
Angle Airborne Camera (WAAC); Int. Arch. of Pho-
togrammetry and Remote Sensing 30(5W1), 26-29.
Gil E., Montenbruck O., Ohlhof T., Schmidhuber M.
(1995): First results on shuttle orbit adjustment using
MOMS-02 imagery; Proc. of the Int. Space Dynamics
Symp., June 19-23, Toulouse, 917—929.
Heipke C., Kornus W., Pfannenstein A. (1994): The eval-
uation of MEOSS airborne 3-line scanner imagery - pro-
cessing chain and results. Int. Arch. of Photogramme-
try and Remote Sensing 30(4), 239-250.
Lanzl F. (1986): The Monocular Electro-Optical Stereo
Scanner (MEOSS) satellite experiment; Int. Arch. of
Photogrammetry and Remote Sensing, 26(1), 617—620.
Lehner M., Drescher A. (1987): MEOSS, Modelling of
short orbit arcs using Brouwer mean elements or poly-
nomials (least squares approximation tests); DFVLR In-
ternal Report, Oberpfaffenhofen.
Light D.L. (ed) (1980): Satellity Photogrammetry; in:
Manual of Photogrammetry, American Society of Pho-
togrammetry, 4th edition, 883-977.
Masaharu H. (1989): Modelling of Short Arc Orbital Con-
straints for Incorporation into Photogrammetric Adjust-
ment of MEOSS Data; DFVLR-FB 89-14, Oberpfaffen-
hofen.
Montenbruck O., Gill ..E., Ohlhof. T. (1994): A
Combined Approach for Mars-94 Orbit Determina-
tion and Photogrammetric Bundle Adjustment; DLR-
Forschungsbericht 94-13, 95 p.
Miller F., Hofmann O., Kaltenecker A. (1994): Digital
Photogrammetric Assembly (DPS) point determination
using airborne three-line camera imagery: practical re-
sults. Int. Arch. of Photogrammetry and Remote Sens-
ing 30(3/2), 592-598.
Murai S., Matsumoto Y., Li X. (1995): Stereoscopic im-
agery with an airborne 3-line scanner (TLS); Int. Arch.
of Photogrammetry and Remote Sensing 30(5W1), 20-
25.
Neukum G., Oberst J., Schwarz G., Flohrer J., Sebastian
I., Jaumann R., Hoffmann H., Carsenty U., Eichentopf
K., Pischel R. (1995): The Multiple Line Scanner Cam-
era Experiment for the Russian Mars96 Mission: Status
Report and Prospects for the Future; in: Photogram-
metric Week ’95, edited by D. Fritsch and D. Hobbie,
Wichmann, Karlsruhe, 45-61.
Ohlhof T. (1995): Lokale, regionale und globale Punktbes-
timmung mit Bild- und Bahninformation der Mars96-
Mission; PhD thesis, Deutsche Geodatische Kommis-
sion, C 445, 139 p.
Sandan R., Barwald W. (1994): A three-line wide-angle
CCD stereo camera for Mars-94 mission; Int. Arch. of
Photogrammetry and Remote Sensing 30(1), 82-86.
Seige P. and D. Meissner D. (1993): MOMS-02: An ad-
vanced high resolution multispectral stereo scanner for
Earth observation; GIS 6(1), 4-11.
Westin T. (1990): Precision Rectification of SPOT Im-
agery; Photogrammetric Engineering and Remote Sens-
ing 56(2), 247-253.