| drdpgr |
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Table of contents
Procedure
DRDPGR ( Derivative of rectangular w.r.t. planetographic )
SUBROUTINE DRDPGR ( BODY, LON, LAT, ALT, RE, F, JACOBI )
Abstract
Compute the Jacobian matrix of the transformation from
planetographic to rectangular coordinates.
Required_Reading
None.
Keywords
COORDINATES
DERIVATIVES
MATRIX
Declarations
IMPLICIT NONE
INCLUDE 'zzctr.inc'
CHARACTER*(*) BODY
DOUBLE PRECISION LON
DOUBLE PRECISION LAT
DOUBLE PRECISION ALT
DOUBLE PRECISION RE
DOUBLE PRECISION F
DOUBLE PRECISION JACOBI ( 3, 3 )
Brief_I/O
VARIABLE I/O DESCRIPTION
-------- --- --------------------------------------------------
BODY I Name of body with which coordinates are associated.
LON I Planetographic longitude of a point (radians).
LAT I Planetographic latitude of a point (radians).
ALT I Altitude of a point above reference spheroid.
RE I Equatorial radius of the reference spheroid.
F I Flattening coefficient.
JACOBI O Matrix of partial derivatives.
Detailed_Input
BODY is the name of the body with which the planetographic
coordinate system is associated.
BODY is used by this routine to look up from the
kernel pool the prime meridian rate coefficient giving
the body's spin sense. See the $Files and $Particulars
header sections below for details.
LON is the planetographic longitude of the input point. This
is the angle between the prime meridian and the meridian
containing the input point. For bodies having prograde
(aka direct) rotation, the direction of increasing
longitude is positive west: from the +X axis of the
rectangular coordinate system toward the -Y axis. For
bodies having retrograde rotation, the direction of
increasing longitude is positive east: from the +X axis
toward the +Y axis.
The earth, moon, and sun are exceptions:
planetographic longitude is measured positive east for
these bodies.
The default interpretation of longitude by this
and the other planetographic coordinate conversion
routines can be overridden; see the discussion in
$Particulars below for details.
Longitude is measured in radians. On input, the range
of longitude is unrestricted.
LAT is the planetographic latitude of the input point. For a
point P on the reference spheroid, this is the angle
between the XY plane and the outward normal vector at
P. For a point P not on the reference spheroid, the
planetographic latitude is that of the closest point
to P on the spheroid.
Latitude is measured in radians. On input, the
range of latitude is unrestricted.
ALT is the altitude of point above the reference spheroid.
Units of ALT must match those of RE.
RE is the equatorial radius of a reference spheroid. This
spheroid is a volume of revolution: its horizontal
cross sections are circular. The shape of the
spheroid is defined by an equatorial radius RE and
a polar radius RP. Units of RE must match those of
ALT.
F is the flattening coefficient =
(RE-RP) / RE
where RP is the polar radius of the spheroid, and the
units of RP match those of RE.
Detailed_Output
JACOBI is the matrix of partial derivatives of the conversion
from planetographic to rectangular coordinates. It
has the form
.- -.
| DX/DLON DX/DLAT DX/DALT |
| DY/DLON DY/DLAT DY/DALT |
| DZ/DLON DZ/DLAT DZ/DALT |
`- -'
evaluated at the input values of LON, LAT and ALT.
Parameters
None.
Exceptions
1) If the body name BODY cannot be mapped to a NAIF ID code,
and if BODY is not a string representation of an integer,
the error SPICE(IDCODENOTFOUND) is signaled.
2) If the kernel variable
BODY<ID code>_PGR_POSITIVE_LON
is present in the kernel pool but has a value other
than one of
'EAST'
'WEST'
the error SPICE(INVALIDOPTION) is signaled. Case
and blanks are ignored when these values are interpreted.
3) If polynomial coefficients for the prime meridian of BODY
are not available in the kernel pool, and if the kernel
variable BODY<ID code>_PGR_POSITIVE_LON is not present in
the kernel pool, the error SPICE(MISSINGDATA) is signaled.
4) If the equatorial radius is non-positive, the error
SPICE(VALUEOUTOFRANGE) is signaled.
5) If the flattening coefficient is greater than or equal to one,
the error SPICE(VALUEOUTOFRANGE) is signaled.
Files
This routine expects a kernel variable giving BODY's prime
meridian angle as a function of time to be available in the
kernel pool. Normally this item is provided by loading a PCK
file. The required kernel variable is named
BODY<body ID>_PM
where <body ID> represents a string containing the NAIF integer
ID code for BODY. For example, if BODY is 'JUPITER', then
the name of the kernel variable containing the prime meridian
angle coefficients is
BODY599_PM
See the PCK Required Reading for details concerning the prime
meridian kernel variable.
The optional kernel variable
BODY<body ID>_PGR_POSITIVE_LON
also is normally defined via loading a text kernel. When this
variable is present in the kernel pool, the prime meridian
coefficients for BODY are not required by this routine. See the
$Particulars section for details.
Particulars
It is often convenient to describe the motion of an object in the
planetographic coordinate system. However, when performing
vector computations it's hard to beat rectangular coordinates.
To transform states given with respect to planetographic
coordinates to states with respect to rectangular coordinates,
one makes use of the Jacobian of the transformation between the
two systems.
Given a state in planetographic coordinates
( lon, lat, alt, dlon, dlat, dalt )
the velocity in rectangular coordinates is given by the matrix
equation:
t | t
(dx, dy, dz) = JACOBI| * (dlon, dlat, dalt)
|(lon,lat,alt)
This routine computes the matrix
|
JACOBI|
|(lon,lat,alt)
In the planetographic coordinate system, longitude is defined
using the spin sense of the body. Longitude is positive to the
west if the spin is prograde and positive to the east if the spin
is retrograde. The spin sense is given by the sign of the first
degree term of the time-dependent polynomial for the body's prime
meridian Euler angle "W": the spin is retrograde if this term is
negative and prograde otherwise. For the sun, planets, most
natural satellites, and selected asteroids, the polynomial
expression for W may be found in a SPICE PCK kernel.
The earth, moon, and sun are exceptions: planetographic longitude
is measured positive east for these bodies.
If you wish to override the default sense of positive longitude
for a particular body, you can do so by defining the kernel
variable
BODY<body ID>_PGR_POSITIVE_LON
where <body ID> represents the NAIF ID code of the body. This
variable may be assigned either of the values
'WEST'
'EAST'
For example, you can have this routine treat the longitude
of the earth as increasing to the west using the kernel
variable assignment
BODY399_PGR_POSITIVE_LON = 'WEST'
Normally such assignments are made by placing them in a text
kernel and loading that kernel via FURNSH.
The definition of this kernel variable controls the behavior of
the SPICELIB planetographic routines
PGRREC
RECPGR
DPGRDR
DRDPGR
It does not affect the other SPICELIB coordinate conversion
routines.
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) Find the planetographic state of the earth as seen from
Mars in the J2000 reference frame at January 1, 2005 TDB.
Map this state back to rectangular coordinates as a check.
Use the meta-kernel shown below to load the required SPICE
kernels.
KPL/MK
File name: drdpgr_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
pck00008.tpc Planet orientation and
radii
naif0009.tls Leapseconds
\begindata
KERNELS_TO_LOAD = ( 'de421.bsp',
'pck00008.tpc',
'naif0009.tls' )
\begintext
End of meta-kernel
Example code begins here.
PROGRAM DRDPGR_EX1
IMPLICIT NONE
C
C SPICELIB functions
C
DOUBLE PRECISION RPD
C
C Local variables
C
DOUBLE PRECISION ALT
DOUBLE PRECISION DRECTN ( 3 )
DOUBLE PRECISION ET
DOUBLE PRECISION F
DOUBLE PRECISION JACOBI ( 3, 3 )
DOUBLE PRECISION LAT
DOUBLE PRECISION LON
DOUBLE PRECISION LT
DOUBLE PRECISION PGRVEL ( 3 )
DOUBLE PRECISION RADII ( 3 )
DOUBLE PRECISION RE
DOUBLE PRECISION RECTAN ( 3 )
DOUBLE PRECISION RP
DOUBLE PRECISION STATE ( 6 )
INTEGER N
C
C Load SPK, PCK, and LSK kernels, use a meta kernel for
C convenience.
C
CALL FURNSH ( 'drdpgr_ex1.tm' )
C
C Look up the radii for Mars. Although we
C omit it here, we could first call BADKPV
C to make sure the variable BODY499_RADII
C has three elements and numeric data type.
C If the variable is not present in the kernel
C pool, BODVRD will signal an error.
C
CALL BODVRD ( 'MARS', 'RADII', 3, N, RADII )
C
C Compute flattening coefficient.
C
RE = RADII(1)
RP = RADII(3)
F = ( RE - RP ) / RE
C
C Look up the geometric state of earth as seen from Mars at
C January 1, 2005 TDB, relative to the J2000 reference
C frame.
C
CALL STR2ET ( 'January 1, 2005 TDB', ET )
CALL SPKEZR ( 'Earth', ET, 'J2000', 'LT+S',
. 'Mars', STATE, LT )
C
C Convert position to planetographic coordinates.
C
CALL RECPGR ( 'MARS', STATE, RE, F, LON, LAT, ALT )
C
C Convert velocity to planetographic coordinates.
C
CALL DPGRDR ( 'MARS', STATE(1), STATE(2), STATE(3),
. RE, F, JACOBI )
CALL MXV ( JACOBI, STATE(4), PGRVEL )
C
C As a check, convert the planetographic state back to
C rectangular coordinates.
C
CALL PGRREC ( 'MARS', LON, LAT, ALT, RE, F, RECTAN )
CALL DRDPGR ( 'MARS', LON, LAT, ALT, RE, F, JACOBI )
CALL MXV ( JACOBI, PGRVEL, DRECTN )
WRITE(*,*) ' '
WRITE(*,*) 'Rectangular coordinates:'
WRITE(*,*) ' '
WRITE(*,*) ' X (km) = ', STATE(1)
WRITE(*,*) ' Y (km) = ', STATE(2)
WRITE(*,*) ' Z (km) = ', STATE(3)
WRITE(*,*) ' '
WRITE(*,*) 'Rectangular velocity:'
WRITE(*,*) ' '
WRITE(*,*) ' dX/dt (km/s) = ', STATE(4)
WRITE(*,*) ' dY/dt (km/s) = ', STATE(5)
WRITE(*,*) ' dZ/dt (km/s) = ', STATE(6)
WRITE(*,*) ' '
WRITE(*,*) 'Ellipsoid shape parameters: '
WRITE(*,*) ' '
WRITE(*,*) ' Equatorial radius (km) = ', RE
WRITE(*,*) ' Polar radius (km) = ', RP
WRITE(*,*) ' Flattening coefficient = ', F
WRITE(*,*) ' '
WRITE(*,*) 'Planetographic coordinates:'
WRITE(*,*) ' '
WRITE(*,*) ' Longitude (deg) = ', LON / RPD()
WRITE(*,*) ' Latitude (deg) = ', LAT / RPD()
WRITE(*,*) ' Altitude (km) = ', ALT
WRITE(*,*) ' '
WRITE(*,*) 'Planetographic velocity:'
WRITE(*,*) ' '
WRITE(*,*) ' d Longitude/dt (deg/s) = ', PGRVEL(1)/RPD()
WRITE(*,*) ' d Latitude/dt (deg/s) = ', PGRVEL(2)/RPD()
WRITE(*,*) ' d Altitude/dt (km/s) = ', PGRVEL(3)
WRITE(*,*) ' '
WRITE(*,*) 'Rectangular coordinates from inverse ' //
. 'mapping:'
WRITE(*,*) ' '
WRITE(*,*) ' X (km) = ', RECTAN(1)
WRITE(*,*) ' Y (km) = ', RECTAN(2)
WRITE(*,*) ' Z (km) = ', RECTAN(3)
WRITE(*,*) ' '
WRITE(*,*) 'Rectangular velocity from inverse mapping:'
WRITE(*,*) ' '
WRITE(*,*) ' dX/dt (km/s) = ', DRECTN(1)
WRITE(*,*) ' dY/dt (km/s) = ', DRECTN(2)
WRITE(*,*) ' dZ/dt (km/s) = ', DRECTN(3)
WRITE(*,*) ' '
END
When this program was executed on a Mac/Intel/gfortran/64-bit
platform, the output was:
Rectangular coordinates:
X (km) = 146039733.67043769
Y (km) = 278546605.40670651
Z (km) = 119750317.58721757
Rectangular velocity:
dX/dt (km/s) = -47.043272004450600
dY/dt (km/s) = 9.0732615496727291
dZ/dt (km/s) = 4.7579169009979010
Ellipsoid shape parameters:
Equatorial radius (km) = 3396.1900000000001
Polar radius (km) = 3376.1999999999998
Flattening coefficient = 5.8860075555255261E-003
Planetographic coordinates:
Longitude (deg) = 297.66765938292673
Latitude (deg) = 20.844504443932596
Altitude (km) = 336531825.52621418
Planetographic velocity:
d Longitude/dt (deg/s) = -8.3577066632519065E-006
d Latitude/dt (deg/s) = 1.5935566850478802E-006
d Altitude/dt (km/s) = -11.211600779360412
Rectangular coordinates from inverse mapping:
X (km) = 146039733.67043760
Y (km) = 278546605.40670651
Z (km) = 119750317.58721757
Rectangular velocity from inverse mapping:
dX/dt (km/s) = -47.043272004450600
dY/dt (km/s) = 9.0732615496727167
dZ/dt (km/s) = 4.7579169009978992
Restrictions
None.
Literature_References
None.
Author_and_Institution
N.J. Bachman (JPL)
J. Diaz del Rio (ODC Space)
B.V. Semenov (JPL)
W.L. Taber (JPL)
Version
SPICELIB Version 1.1.1, 12-AUG-2021 (JDR)
Edited the header to comply with NAIF standard..
Modified code example to use meta-kernel to load kernels.
SPICELIB Version 1.1.0, 21-SEP-2013 (BVS)
Updated to save the input body name and ZZBODTRN state counter
and to do name-ID conversion only if the counter has changed.
Updated to call LJUCRS instead of CMPRSS/UCASE.
SPICELIB Version 1.0.0, 26-DEC-2004 (NJB) (WLT)
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Fri Dec 31 18:36:14 2021