| dvsep |
|
Table of contents
Procedure
DVSEP ( Derivative of separation angle )
DOUBLE PRECISION FUNCTION DVSEP ( S1, S2 )
Abstract
Calculate the time derivative of the separation angle between
two input states, S1 and S2.
Required_Reading
None.
Keywords
DERIVATIVES
GEOMETRY
Declarations
IMPLICIT NONE
DOUBLE PRECISION S1 (6)
DOUBLE PRECISION S2 (6)
Brief_I/O
VARIABLE I/O DESCRIPTION
-------- --- --------------------------------------------------
S1 I State vector of the first body.
S2 I State vector of the second body.
The function returns the time derivative of the separation angle
between the two input states, S1 and S2.
Detailed_Input
S1,
S2 are, respectively, the state vector of the first and
second target bodies as seen from the observer.
An implicit assumption exists that both states lie in the
same reference frame with the same observer for the same
epoch. If this is not the case, the numerical result has
no meaning.
Detailed_Output
The function returns the double precision value of the time
derivative of the angular separation between S1 and S2.
Parameters
None.
Exceptions
1) If numeric overflow and underflow cases are detected, an error
is signaled by a routine in the call tree of this routine.
2) If called in 'RETURN' mode, the function returns 0.
3) Linear dependent position components of S1 and S1 constitutes
a non-error exception. The function returns 0 for this case.
Files
None.
Particulars
In this discussion, the notation
< V1, V2 >
indicates the dot product of vectors V1 and V2. The notation
V1 x V2
indicates the cross product of vectors V1 and V2.
To start out, note that we need consider only unit vectors,
since the angular separation of any two non-zero vectors
equals the angular separation of the corresponding unit vectors.
Call these vectors U1 and U2; let their velocities be V1 and V2.
For unit vectors having angular separation
THETA
the identity
|| U1 x U1 || = ||U1|| * ||U2|| * sin(THETA) (1)
reduces to
|| U1 x U2 || = sin(THETA) (2)
and the identity
| < U1, U2 > | = || U1 || * || U2 || * cos(THETA) (3)
reduces to
| < U1, U2 > | = cos(THETA) (4)
Since THETA is an angular separation, THETA is in the range
0 : Pi
Then letting s be +1 if cos(THETA) > 0 and -1 if cos(THETA) < 0,
we have for any value of THETA other than 0 or Pi
2 1/2
cos(THETA) = s * ( 1 - sin (THETA) ) (5)
or
2 1/2
< U1, U2 > = s * ( 1 - sin (THETA) ) (6)
At this point, for any value of THETA other than 0 or Pi,
we can differentiate both sides with respect to time (T)
to obtain
2 -1/2
< U1, V2 > + < V1, U2 > = s * (1/2)(1 - sin (THETA))
* (-2) sin(THETA)*cos(THETA)
* d(THETA)/dT (7a)
Using equation (5), and noting that s = 1/s, we can cancel
the cosine terms on the right hand side
-1
< U1, V2 > + < V1, U2 > = (1/2)(cos(THETA))
* (-2) sin(THETA)*cos(THETA)
* d(THETA)/dT (7b)
With (7b) reducing to
< U1, V2 > + < V1, U2 > = - sin(THETA) * d(THETA)/dT (8)
Using equation (2) and switching sides, we obtain
|| U1 x U2 || * d(THETA)/dT = - < U1, V2 > - < V1, U2 > (9)
or, provided U1 and U2 are linearly independent,
d(THETA)/dT = ( - < U1, V2 > - < V1, U2 > ) / ||U1 x U2|| (10)
Note for times when U1 and U2 have angular separation 0 or Pi
radians, the derivative of angular separation with respect to
time doesn't exist. (Consider the graph of angular separation
with respect to time; typically the graph is roughly v-shaped at
the singular points.)
Examples
The numerical results shown for this example may differ across
platforms. The results depend on the SPICE kernels used as
input, the compiler and supporting libraries, and the machine
specific arithmetic implementation.
1) Calculate the time derivative of the angular separation of
the Earth and Moon as seen from the Sun at a given time.
Use the meta-kernel shown below to load the required SPICE
kernels.
KPL/MK
File name: dvsep_ex1.tm
This meta-kernel is intended to support operation of SPICE
example programs. The kernels shown here should not be
assumed to contain adequate or correct versions of data
required by SPICE-based user applications.
In order for an application to use this meta-kernel, the
kernels referenced here must be present in the user's
current working directory.
The names and contents of the kernels referenced
by this meta-kernel are as follows:
File name Contents
--------- --------
de421.bsp Planetary ephemeris
pck00010.tpc Planet orientation and
radii
naif0012.tls Leapseconds
\begindata
KERNELS_TO_LOAD = ( 'de421.bsp',
'pck00010.tpc',
'naif0012.tls' )
\begintext
End of meta-kernel
Example code begins here.
PROGRAM DVSEP_EX1
IMPLICIT NONE
DOUBLE PRECISION ET
DOUBLE PRECISION LT
DOUBLE PRECISION DSEPT
DOUBLE PRECISION STATEE (6)
DOUBLE PRECISION STATEM (6)
INTEGER STRLEN
PARAMETER ( STRLEN = 64 )
CHARACTER*(STRLEN) BEGSTR
DOUBLE PRECISION DVSEP
C
C Load kernels.
C
CALL FURNSH ('dvsep_ex1.tm')
C
C An arbitrary time.
C
BEGSTR = 'JAN 1 2009'
CALL STR2ET( BEGSTR, ET )
C
C Calculate the state vectors Sun to Moon, and
C Sun to Earth at ET.
C
C
CALL SPKEZR ( 'EARTH', ET, 'J2000', 'NONE', 'SUN',
. STATEE, LT)
CALL SPKEZR ( 'MOON', ET, 'J2000', 'NONE', 'SUN',
. STATEM, LT)
C
C Calculate the time derivative of the angular separation
C of the Earth and Moon as seen from the Sun at ET.
C
DSEPT = DVSEP( STATEE, STATEM )
WRITE(*,*) 'Time derivative of angular'
WRITE(*,*) ' separation (rad/sec): ', DSEPT
END
When this program was executed on a Mac/Intel/gfortran/64-bit
platform, the output was:
Time derivative of angular
separation (rad/sec): 3.8121193666132696E-009
Restrictions
None.
Literature_References
None.
Author_and_Institution
J. Diaz del Rio (ODC Space)
E.D. Wright (JPL)
Version
SPICELIB Version 2.0.1, 06-JUL-2021 (JDR)
Edited the header to comply with NAIF standard. Added problem
statement and meta-kernel to the example. Modified output to
comply with maximum line length of header comments.
SPICELIB Version 2.0.0, 21-MAR-2014 (EDW)
Reimplemented algorithm using ZZDIV.
SPICELIB Version 1.0.1, 15-MAR-2010 (EDW)
Trivial header format clean-up.
SPICELIB Version 1.0.0, 31-MAR-2009 (EDW)
|
Fri Dec 31 18:36:17 2021