Data Set Information
|
DATA_SET_NAME |
LP MOON SPACECRAFT TRAJECTORY V1.0
|
DATA_SET_ID |
LP-L-6-TRAJECTORY-V1.0
|
NSSDC_DATA_SET_ID |
|
DATA_SET_TERSE_DESCRIPTION |
Trajectory data for the Lunar
Prospector spacecraft in Selenographic, SSE, GSE, and GSM coordinates.
Dataset covers dates 1998-01-16 to 1999-07-29.
|
DATA_SET_DESCRIPTION |
Data Set Overview
=================
The Lunar Prospector spacecraft trajectory data set consists of
spacecraft position determinations in numerous coordinate systems
at one minute intervals. The data set also contains the spacecraft
velocity as a function of time. This data set is derived by using
the spacecraft position data set from the Lunar Prospector level
zero data archive (LP-L-6-POSITION-V1.0). The SPICE SPK kernel
LP_EPHEM.TSP that is included on the archive volume provides
ephemeris data for the Sun, Earth, and Moon. These data are combined
with the Lunar Prospector location relative to the Moon in order
to generate trajectory data that will facilitate the analysis of
both the magnetometer and the electron reflectometer data sets.
Each file in the spacecraft trajectory data set covers one month of
time.
Science Objectives
==================
The Lunar Prospector science objectives relevant to this data set are
to map the Moon's surface composition and its magnetic field, and to
determine the frequency and location of gas release events. A
special emphasis of the science objectives is to search for polar
water ice deposits [BINDERETAL1998]. The spacecraft position data
are used to locate where on the Moon science data were acquired.
Coordinate Systems
==================
Selenographic: These data are a repeat of the values generated by
the Goddard Flight Dynamics Analysis Branch for the level zero data.
The selenographic coordinate system provided is an east longitude
system where the prime meridian is defined in [DAVIESETAL1994]. A
negligible amount of flattening (1x10**-30) is used for the Moon.
Thus, selenographic latitude is nearly equal to selenocentric
latitude with almost no error. The mean radius and GM of the Moon
used to generate this data set are 1738 km and 4902.8014 km**3/s**2,
respectively. Both spherical (SG) and Cartesian (SEL) representations
of the selenographic coordinate system are provided. In the Cartesian
representation, the Z-axis is aligned with the lunar spin axis,
positive in the direction of angular momentum. The X-axis lies in
the equatorial plane and points in the direction of the prime
meridian. Y completes the right-handed set.
Selenocentric Solar Ecliptic (SSE): The SSE coordinate system has
its X-axis along the instantaneous Moon-Sun line, positive towards
the Sun. The Z-axis is parallel to the upward normal to the Earth's
ecliptic plane, and Y completes the right-handed set. Distances are
measured from the lunar center of mass and are reported in units
of kilometers.
Geocentric Solar Ecliptic (GSE): The GSE coordinate system has
its X-axis along the instantaneous Earth-Sun line, positive towards
the Sun. The Z-axis is parallel to the upward normal to the Earth's
ecliptic plane, and Y completes the right-handed set. Distances are
measured from the Earth center of mass and are reported in units
of Earth radii where 1 Re = 6372 km.
Geocentric Solar Magnetospheric (GSM): The GSM coordinate system has
its X-axis along the instantaneous Earth-Sun line, positive towards
the Sun (same as GSE X-axis!). The X-Z plane is defined to contain
the the Earth's dipole (passes through 78.565 deg North, 69.761 deg
West). Y completes the right-handed set. Distances are measured from
the Earth center of mass and are reported in units of Earth radii
where 1 Re = 6372 km.
Definitions of the GSE and GSM coordinate systems come from
[RUSSELL1971]. The Earth's dipole location used in the GSM coordinate
system definition is based on the 1970 IGRF model as stated in that
reference.
|
DATA_SET_RELEASE_DATE |
2000-07-25T00:00:00.000Z
|
START_TIME |
1998-01-16T12:00:00.000Z
|
STOP_TIME |
1999-07-31T10:10:00.000Z
|
MISSION_NAME |
LUNAR PROSPECTOR
|
MISSION_START_DATE |
1995-01-01T12:00:00.000Z
|
MISSION_STOP_DATE |
1999-07-31T12:00:00.000Z
|
TARGET_NAME |
MOON
|
TARGET_TYPE |
SATELLITE
|
INSTRUMENT_HOST_ID |
LP
|
INSTRUMENT_NAME |
LP ENGINEERING
|
INSTRUMENT_ID |
ENG
|
INSTRUMENT_TYPE |
N/A
|
NODE_NAME |
Planetary Plasma Interactions
|
ARCHIVE_STATUS |
ARCHIVED
|
CONFIDENCE_LEVEL_NOTE |
Confidence Level Overview
=========================
Error bars are not provided with the original spacecraft position
data set. All values in this data set are reported to the nearest
kilometer. The actual error bars are probably larger than 1 km and
different in the 'along track', cross-track', and 'altitude'
directions.
Data Coverage and Quality
=========================
Spacecraft position data exist for the entire Lunar Prospector
Primary and Extended Missions.
|
CITATION_DESCRIPTION |
Joy, S.P., LP-L-6-TRAJECTORY-V1.0,
LP MOON SPACECRAFT TRAJECTORY V1.0,
NASA Planetary Data System, 2000.
|
ABSTRACT_TEXT |
Trajectory data for the Lunar
Prospector spacecraft in Selenographic, SSE, GSE, and GSM coordinates.
Dataset covers dates 1998-01-16 to 1999-07-29.
|
PRODUCER_FULL_NAME |
STEVEN P. JOY
|
SEARCH/ACCESS DATA |
Planetary Plasma Interactions Website
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