Full text: Technical Commission IV (B4)

> XXXIX-B4, 2012 
-Zoom mode. The PDS 
evel 1 calibrated byt 
2 map-projected (CDR- 
o date. The volume of 
other products contain 
because of redundancy 
zhly 3 orders of magni- 
Mini-RF was added to 
istration in 2005. 
IS 
vious section include 
ll as geometrically raw 
^ majority of these 
r at best semicontrolled. 
DTMs, and other map 
among the controlled 
taset, for which orbit 
S have been adjusted to 
where altimetric profiles 
re dense gridded data 
poles (Mazarico et al. 
LA, and the ability of its 
5 well as elevations, this 
ence for other mapping 
Iso being corrected by 
ough so far on a local 
ingly, studies exploring 
of the altimetry from 
ium et al. 2012) have 
d using the altimetric 
ntrolled image products 
| of M? data based on 
production of polar (Lee 
(Rosiek et al. 2012) 
iges. The polar mosaics 
, — the largest controlled 
covering the lunar polar 
xel. Much of the latter 
yA Lunar Mapping and 
|. 2009; data accessible 
nasa.gov/). A variety of 
is such as orthoimages 
Ms from Chandrayaan-1 
Chang’e-1 CCD images 
es (see Beyer et al. 2011 
producing such DTMs 
nsorship, and Rosiek et 
lore recent summaries). 
Chandrayaan-1 Mini-RF 
(Kirk et al. 2011) and 
is currently under way 
RENT DATA 
nd exploration, the lunar 
st be co-registered in a 
)nly such an effort will 
yn, and error analysis of 
ie full comparative and 
ummary in this section 
. the development and 
a products. 
| from all lunar missions 
mon frame via geodetic 
c, radargrammetric, and 
s rigorous process will 
ecessary to generate the 
al DTM. Such a model 
ic calibration and ortho- 
nages are brought into 
International Archives of the Photogrammetry, Remote Sensin 
g and Spatial Information Sciences, Volume XXXIX-B4, 2012 
XXII ISPRS Congress, 25 August — 01 September 2012, Melbourne, Australia 
common frame and a common DTM is in use, the datasets can 
be converted into information, primarily in the form of useful 
cartographic products. Such products are essential for 
addressing lunar science and exploration goals at the highest 
possible level of accuracy. As a result of the merging process, 
the accuracy level of such products will be known and 
documented, which will be critical for the comparison of the 
products and for their use in future decision making. 
In order to meet the increasing needs of the science and 
exploration communities, datasets must be comparable at the 
pixel level with accuracy on the order of tenths of a pixel 
required for color and spectral data. Such accuracy is only 
possible with geodetically controlled products that are 
orthorectified onto DTMs with resolutions approaching those of 
the output image products. 
Detailed arguments have been put forth that more extensive 
cartographic efforts are needed to exploit past missions fully 
and to prepare properly for future missions (Archinal et al. 
2007; Kirk et al. 2008). The NASA Advisory Council has 
recognized the importance of such processing, recommending 
that all lunar datasets be geodetically controlled (NAC, 2007). 
The IAU Working Group on Cartographic Coordinates and 
Rotational Elements has also recently recognized the value of 
controlled products (Archinal et al. 2011, recommendation 1) 
and the need to generate them from new mission datasets. As 
noted in Section 2, controlled cartographic products from recent 
missions are greatly outnumbered by uncontrolled products. 
The number of controlled products is growing and efforts to 
combine data from multiple missions have begun (e.g., Iz et al. 
2011; Shum et al. 2012) but given the volume and complexity 
of the data it is clear that a massive effort will be required to 
control even the most critical of these new large lunar datasets. 
Given the funding constraints on recent major international 
missions to the Moon and the need to register datasets from 
multiple missions, an international co-operative project would 
greatly facilitate accomplishment of the work described here. If 
necessary, significant progress could be made even without 
requiring the release of raw data from all missions. Joint efforts 
at mapping would be a good first step that would greatly 
encourage and facilitate broader international cooperation in the 
exploration of the Moon. 
In the following subsections we describe the need for 
controlling the data, for generating a merged global DTM, and 
for establishing a common reference frame. Basic high 
resolution datasets are listed that need to be connected initially 
and principles of processing are described to outline in what 
order and how datasets could be registered to each other and a 
common frame. Some of the many and difficult challenges in 
accomplishing such work are briefly considered. 
31 The Need for Geodetic Control 
The only way to connect/register/compare data with quantified 
precision and accuracy is to geodetically (usually photo- 
grammetrically) process the data into controlled products. 
Otherwise the uncertainties in the comparison of datasets 
undermine their synergistic value. Users always want the best 
precision and accuracy possible and require that they be 
quantified. Such knowledge is critical for mineralogic, geologic, 
and other scientific investigations and exploration purposes 
Such as site selection, landing, and landed operations. Con- 
tolling any single dataset provides many benefits including: (a) 
the best method of removal of mosaic seams for qualitative 
Work; (b) proper orthometric projection of data (i.e., registration 
of Images to topography in order to make or match existing 
mosaics and maps); (c) registration of multispectral data, which 
Is essential to do at subpixel precision to avoid fringing 
artifacts; and (d) proper photometric correction of data. The 
Value of such control increases exponentially when multiple 
datasets are considered, so it is essential that this work be 
Planned for and done with new lunar data. Geodetic control 
adds substantial value to the data, especially relative to the cost 
of data collection and the immense risk that future surface 
46 
missions may fail if the maps used to evaluate landing site 
safety or plan their operations are insufficiently accurate. 
3.2 The Need for Global Topography 
As noted in Section 2, new global DTMs have recently been 
produced from Kaguya (Araki et al. 2009), LOLA (Smith et al. 
2010), and Chang’e-1 (Li et al. 2010) altimetry, as well as 
Kaguya TC (Haruyama et al. 2012) and LROC WAC (Scholten 
et al. 2011) stereo imagery. As revolutionary and scientifically 
valuable as these models are, there is still a need for global 
topographic modeling at higher resolution and accuracy. For 
example, the laser altimetry models have substantial longi- 
tudinal data gaps at mid- and particularly equatorial latitudes. 
The WAC stereo DTM is based on ~100 m resolution images 
that, although aligned with LOLA Team derived spacecraft 
position information, are uncontrolled and may have errors 
comparable to their resolution. These existing global models are 
therefore insufficient for the orthoprojection of high resolution 
images at or even near the resolution of such data. They are also 
insufficient for the orthoprojection, slope correction, and 
calibration of medium resolution (100 m/pixel or more) color, 
multispectral, or infrared data (e.g., Kaguya MI and SP, LRO 
WAC and DLRE, Chandrayaan-I M’). Correction of slope 
based photometric effects requires topographic data with 
horizontal resolution at the image pixel scale or less and vertical 
precision on the order of a tenth of a pixel or less. Such 
photometric correction has been shown to affect the 
compositional interpretation of spectral data at the 5% level and 
significantly affect geologic interpretations of spectral 
variability (Robinson and Jolliff 2002). 
A high-resolution, global DTM is not only needed to process 
global datasets in preparation for scientific analysis, it is critical 
for successfully planning and conducting robotic and human 
mission operations on the Moon. Even higher resolution DTMs 
are needed to process local to regional high-resolution data. 
Such DTMs can be generated from the combination of the 
altimeter data and stereo data, particularly (in order from 
highest to lowest resolution) NAC, Apollo, TMC, CCD-2, TC. 
MI, and LRO Mini-RF imagery. 
3.3 What System and Frame? 
The recommended coordinate system for the Moon (Archinal et 
al. 2011; LRO & LGCWG 2008) is the mean Earth / polar axis 
(ME) system, and the recommended way to access it is via the 
JPL DE 421 ephemerides, with an appropriate rotation to the 
ME system. The recommended mean radius for the Moon is 
1737.4 km (Archinal et al. 2011; LRO & LGCWG, 2008), and 
fortunately most instrument teams and missions have adopted 
these recommendations. The real issue then becomes using or 
creating a reference frame within that coordinate system to 
which datasets can be referred. Currently the best lunar 
reference frames are those derived from Lunar Laser Ranging 
(LLR). These frames have coordinate System accuracies 
approaching the decimeter to centimeter level, but only for the 5 
existing LLR targets. It will be necessary to tie the other 
datasets into an LLR frame or one based on it. 
3.4 What Datasets? 
Noted above are some of the highest density or resolution 
altimetric and stereo datasets that can be used to build a 
fundamental lunar reference frame and uniform global DTM. 
Other required data include spacecraft geometric (“SPICE” — 
Acton 1999 —or similar) data and a lunar gravity model (ideally 
incorporating the results from the GRAIL mission). Once such a 
frame and model are established, all lunar data can be tied to 
them, including the recent mission data described in Section 2, 
and data from earlier missions such as Lunar Orbiter, Apollo, 
Clementine, and Lunar Prospector. 
3.5 Processing Principles 
Some flexibility exists concerning the order in which data 
should be processed, and in which algorithms, software, and 
1 
 
	        
Waiting...

Note to user

Dear user,

In response to current developments in the web technology used by the Goobi viewer, the software no longer supports your browser.

Please use one of the following browsers to display this page correctly.

Thank you.