Index of Functions: A  B  C  D  E  F  G  H  I  J  K  L  M  N  O  P  Q  R  S  T  U  V  W  X 
Index Page
dvsep

Table of contents
Procedure
Abstract
Required_Reading
Keywords
Declarations
Brief_I/O
Detailed_Input
Detailed_Output
Parameters
Exceptions
Files
Particulars
Examples
Restrictions
Literature_References
Author_and_Institution
Version

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