The relative ephemeris of the assigned
object with respect to the primary object, expressed in Cartesian
components, as a function of time. The relative ephemeris is
computed with respect to two rotating frames, the RIC (Radial,
In-Track, Cross-Track) frame and the NTC (Normal, Tangential, and
Cross-Track) frames, that are defined using the primary's
ephemeris. Cross-track refers to the direction perpendicular to the
position and inertial velocity; in-track refers to the direction
perpendicular to both the radial and cross-track (positive in the
direction of motion); tangential refers to the direction along the
velocity vector; and normal refers to the direction perpendicular
to the velocity and cross-track directions (positive outward along
radial).
Name |
Dimension |
Type |
Description |
Time |
DateFormat |
Real Number |
Time. |
Radial |
DistanceUnit |
Real Number |
The radial component of the relative position
vector. |
In-Track |
DistanceUnit |
Real Number |
The in-track component of the relative position
vector. |
Cross-Track |
DistanceUnit |
Real Number |
The cross-track component of the relative position
vector. |
Range |
DistanceUnit |
Real Number |
The range (i.e., distance between the primary and
secondary object) at the given time. |
Radial Rate |
Rate |
Real Number |
The radial component of the relative velocity
vector as observed in the RIC rotating frame. |
In-Track Rate |
Rate |
Real Number |
The in-track component of the relative velocity
vector as observed in the RIC rotating frame. |
Cross-Track Rate |
Rate |
Real Number |
The cross-track component of the relative velocity
vector as observed in the RIC rotating frame. |
Range Rate |
Rate |
Real Number |
The rate of change of the magnitude of the relative
position vector. This is computed using the analytical formula
dot_product(relative_position_vector, relative_velocity_vector) /
magnitude(relative_position_vector). This is an exact formula when
the velocity is the derivative of position. Some propagators (e.g.,
SGP4, J2Perturbation, J4Perturbation), however, produce ephemerides
where the velocity is not exactly the derivative of position so
that this formula does not compute the derivative of range exactly
in such cases. |
Range Rate
Numerical |
Rate |
Real Number |
The rate of change of the magnitude of the relative
position vector. This is computed using numerical differentiation
of the range. The central difference will be used for interior
points; forward or backward differences will be used at ephemeris
start and stop times. |
Range Rate Dot |
Acceleration |
Real Number |
The time derivative of the range rate, as evaluated
using the analytical formula. |
Range
Rate Dot Numerical |
Acceleration |
Real Number |
The time derivative of the range rate, as evaluated
using numerical differentiation. |
Tangential |
DistanceUnit |
Real Number |
The tangential component of the relative position
vector. |
Tangential Rate |
Rate |
Real Number |
The tangential component of the relative velocity
vector as observed in the NTC rotating frame. |
Normal |
DistanceUnit |
Real Number |
The normal component of the relative position
vector. |
Normal Rate |
Rate |
Real Number |
The normal component of the relative velocity
vector as observed in the NTC rotating frame. |
Time Difference |
TimeUnit |
Real Number |
Alternative measure for in-track position
difference, computed as as duration. The duration is computed by
dividing the in-track component of the relative position vector by
the inertial velocity of the primary object. |
SpeedRelToRICFrame |
Rate |
Real Number |
The magnitude of the relative velocity vector, as
observed in the RIC rotating frame. |
Radial Vel Diff |
Rate |
Real Number |
The radial component of the vector difference
between the assigned object's and the primary's inertial
velocities. |
In-Track Vel
Diff |
Rate |
Real Number |
The in-track component of the vector difference
between the assigned object's and the primary's inertial
velocities. |
Cross-Track
Vel Diff |
Rate |
Real Number |
The cross-track component of the vector difference
between the assigned object's and the primary's inertial
velocities. |
From Object |
DistanceUnit |
Text |
The class name and name of the From-object. |
To Object |
DistanceUnit |
Text |
The class name and name of the To-object. |
Position Cov
Sigma |
Unitless |
Real Number |
Position difference measured in terms of the
position covariance. Reports N where the current relative position
vector lies on a N sigma ellipsoid, where the ellipsoid if obtained
from the position covariance of the primary satellite. This can
only be computed if position covariance is available. |
Position Combined Cov Sigma |
Unitless |
Real Number |
Position difference measured in terms of the
combined position covariance of primary and target satellites.
Reports N where the current relative position vector lies on an N
sigma ellipsoid, where the ellipsoid is obtained from the sum of
the covariances matrices of the two objects. This can only be
computed if position covariance is available. |