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Table of contents
Procedure
LTIME ( Light Time )
SUBROUTINE LTIME ( ETOBS, OBS, DIR, TARG, ETTARG, ELAPSD )
Abstract
Compute the transmission (or reception) time of a signal at a
specified target, given the reception (or transmission) time at a
specified observer. Also return the elapsed time between
transmission and reception.
Required_Reading
None.
Keywords
SPK
Declarations
IMPLICIT NONE
DOUBLE PRECISION ETOBS
INTEGER OBS
CHARACTER*(2) DIR
INTEGER TARG
DOUBLE PRECISION ETTARG
DOUBLE PRECISION ELAPSD
Brief_I/O
VARIABLE I/O DESCRIPTION
-------- --- --------------------------------------------------
ETOBS I Epoch of a signal at some observer.
OBS I NAIF ID of some observer.
DIR I Direction the signal travels ( '->' or '<-' ).
TARG I NAIF ID of the target object.
ETTARG O Epoch of the signal at the target.
ELAPSD O Time between transmit and receipt of the signal.
Detailed_Input
ETOBS is an epoch expressed as ephemeris seconds past J2000
TDB. This is the time at which an electromagnetic signal
is "at" the observer.
OBS is the NAIF ID of some observer.
DIR is the direction the signal travels. The
acceptable values are '->' and '<-'. When
you read the calling sequence from left to
right, the "arrow" given by DIR indicates
which way the electromagnetic signal is traveling.
If the argument list reads as below,
..., OBS, '->', TARG, ...
the signal is traveling from the observer to the
target.
If the argument reads as
..., OBS, '<-', TARG
the signal is traveling from the target to
the observer.
TARG is the NAIF ID of the target.
Detailed_Output
ETTARG is the epoch expressed as ephemeris seconds past J2000
TDB at which the electromagnetic signal is "at" the
target body.
Note ETTARG is computed using only Newtonian
assumptions about the propagation of light.
ELAPSD is the number of ephemeris seconds (TDB) between
transmission and receipt of the signal.
ELAPSD is computed as:
ELAPSD = DABS( ETOBS - ETTARG )
Parameters
None.
Exceptions
1) If DIR is not one of '->' or '<-', the error
SPICE(BADDIRECTION) is signaled. In this case
ETTARG and ELAPSD will not be altered from their
input values.
2) If insufficient ephemeris information is available to
compute the outputs ETTARG and ELAPSD, or if observer
or target is not recognized, an error is signaled
by a routine in the call tree of this routine.
In this case, the value of ETTARG will be set to ETOBS
and ELAPSD will be set to zero.
Files
None.
Particulars
Suppose a radio signal travels between two solar system
objects. Given an ephemeris for the two objects, which way
the signal is traveling, and the time when the signal is
"at" at one of the objects (the observer OBS), this routine
determines when the signal is "at" the other object (the
target TARG). It also returns the elapsed time between
transmission and receipt of the signal.
Examples
Example 1.
----------
Suppose a signal is transmitted at time ET from the Goldstone
tracking site (id-code 399001) to a spacecraft whose id-code
is -77.
signal traveling to spacecraft
* -._.-._.-._.-._.-._.-._.-._.-._.-> *
Goldstone (OBS=399001) Spacecraft (TARG = -77)
at epoch ETOBS(given) at epoch ETTARG(unknown)
Assuming that all of the required SPICE kernels have been
loaded, the code fragment below shows how to compute the
time (ARRIVE) at which the signal arrives at the spacecraft
and how long (HOWLNG) it took the signal to reach the spacecraft.
(Note that we display the arrival time as the number of seconds
past J2000.)
OBS = 399001
TARG = -77
ETOBS = ET
CALL LTIME ( ETOBS, OBS, '->', TARG, ARRIVE, HOWLNG )
CALL ETCAL
WRITE (*,*) 'The signal arrived at time: ', ARRIVE
WRITE (*,*) 'It took ', HOWLNG, ' seconds to get there.'
Example 2.
----------
Suppose a signal is received at the Goldstone tracking sight
at epoch ET from the spacecraft of the previous example.
signal sent from spacecraft
* <-._.-._.-._.-._.-._.-._.-._.-._.- *
Goldstone (OBS=399001) Spacecraft (TARG = -77)
at epoch ETOBS(given) at epoch ETTARG(unknown)
Again assuming that all the required kernels have been loaded
the code fragment below computes the epoch at which the
signal was transmitted from the spacecraft.
OBS = 399001
TARG = -77
ETOBS = ET
CALL LTIME ( ETOBS, OBS, '<-', TARG, SENT, HOWLNG )
CALL ETCAL
WRITE (*,*) 'The signal was transmitted at: ', SENT
WRITE (*,*) 'It took ', HOWLNG, ' seconds to get here.'
EXAMPLE 3
---------
Suppose there is a transponder on board the spacecraft of
the previous examples that transmits a signal back to the
sender exactly 1 microsecond after a signal arrives at
the spacecraft. If we send a signal from Goldstone
to the spacecraft and wait to receive it at Canberra.
What will be the epoch at which the return signal arrives
in Canberra? ( The id-code for Canberra is 399002 ).
Again, assuming we've loaded all the necessary kernels,
the fragment below will give us the answer.
GSTONE = 399001
SC = -77
CANBER = 399002
ETGOLD = ET
CALL LTIME ( ETGOLD, GSTONE, '->', SC, SCGET, LT1 )
Account for the microsecond delay between receipt and transmit
SCSEND = SCGET + 0.000001
CALL LTIME ( SCSEND, SC, '->', CANBER, ETCANB, LT2 )
RNDTRP = ETCANB - ETGOLD
WRITE (*,*) 'The signal arrives in Canberra at: ', ETCANB
WRITE (*,*) 'Round trip time for the signal was: ', RNDTRP
Restrictions
None.
Literature_References
None.
Author_and_Institution
J. Diaz del Rio (ODC Space)
W.L. Taber (JPL)
E.D. Wright (JPL)
Version
SPICELIB Version 1.1.3, 26-OCT-2021 (JDR)
Edited the header to comply with NAIF standard.
SPICELIB Version 1.1.2, 22-SEP-2004 (EDW)
Placed Copyright after $Abstract.
SPICELIB Version 1.1.1, 18-NOV-1996 (WLT)
Errors in the $Examples section were corrected.
SPICELIB Version 1.1.0, 10-JUL-1996 (WLT)
Added Copyright Notice to the header.
SPICELIB Version 1.0.0, 10-NOV-1995 (WLT)
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Fri Dec 31 18:36:32 2021