Table of contents
CSPICE_DRDPGR computes the Jacobian matrix of the transformation
from planetographic to rectangular coordinates.
Given:
body the name of the body with which the planetographic coordinate
system is associated.
[1,c1] = size(body); char = class(body)
or
[1,1] = size(body); cell = class(body)
`body' is used by this routine to look up from the kernel
pool the prime meridian rate coefficient giving the body's
spin sense.
lon the planetographic longitude(s) of the input point(s).
[1,n] = size(lon); double = class(lon)
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 the planetographic latitude(s) of the input point(s).
[1,n] = size(lat); double = class(lat)
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 the altitude(s) of point(s) above the reference spheroid.
[1,n] = size(alt); double = class(alt)
Units of `alt' must match those of `re'.
re the equatorial radius of a reference spheroid.
[1,1] = size(re); double = class(re)
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 the flattening coefficient
f = (re-rp) / re
where `rp' is the polar radius of the spheroid.
[1,1] = size(f); double = class(f)
The units of `rp' match those of `re'. (More importantly
rp = re*(1-f) )
the call:
[jacobi] = cspice_drdpgr( body, lon, lat, alt, re, f )
returns:
jacobi the matrix(es) of partial derivatives of the conversion from
planetographic to rectangular coordinates.
If [1,1] = size(lon) then [3,3] = size(jacobi)
If [1,n] = size(lon) then [3,3,n] = size(jacobi)
double = class(jacobi)
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'.
`jacobi' returns with the same vectorization measure (N)
as `lon', `lat' and `alt'.
None.
Any numerical results shown for this example may differ between
platforms as the results depend on the SPICE kernels used as input
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
--------- --------
de405.bsp Planetary ephemeris
pck00008.tpc Planet orientation and
radii
naif0007.tls Leapseconds
\begindata
KERNELS_TO_LOAD = ( 'de405.bsp',
'pck00008.tpc',
'naif0007.tls' )
\begintext
End of meta-kernel
Example code begins here.
function drdpgr_ex1()
%
% Load SPK, PCK, and LSK kernels, use a meta kernel for
% convenience.
%
cspice_furnsh( 'drdpgr_ex1.tm' );
%
% Look up the radii for Mars. Although we
% omit it here, we could first call badkpv_c
% to make sure the variable BODY499_RADII
% has three elements and numeric data type.
% If the variable is not present in the kernel
% pool, bodvrd_c will signal an error.
%
[radii] = cspice_bodvrd( 'MARS', 'RADII', 3 );
%
% Compute flattening coefficient.
%
re = radii(1);
rp = radii(3);
f = ( re - rp ) / re;
%
% Look up the geometric state of earth as seen from Mars at
% January 1, 2005 TDB, relative to the J2000 reference
% frame.
%
[et] = cspice_str2et( 'January 1, 2005 TDB' );
[state, lt] = cspice_spkezr( 'Earth', et, 'J2000', ...
'LT+S', 'Mars' );
%
% Convert position to planetographic coordinates.
%
[lon, lat, alt] = cspice_recpgr( 'mars', state(1:3), re, f );
%
% Convert velocity to planetographic coordinates.
%
[jacobi] = cspice_dpgrdr( 'MARS', state(1), state(2), ...
state(3), re, f );
pgrvel = jacobi * state(4:6);
%
% As a check, convert the planetographic state back to
% rectangular coordinates.
%
[rectan] = cspice_pgrrec( 'mars', lon, lat, alt, re, f );
[jacobi] = cspice_drdpgr( 'mars', lon, lat, alt, re, f );
drectn = jacobi * pgrvel;
fprintf( '\n' )
fprintf( 'Rectangular coordinates:\n' )
fprintf( '\n' )
fprintf( ' X (km) = %17.8e\n', state (1) )
fprintf( ' Y (km) = %17.8e\n', state (2) )
fprintf( ' Z (km) = %17.8e\n', state (3) )
fprintf( '\n' )
fprintf( 'Rectangular velocity:\n' )
fprintf( '\n' )
fprintf( ' dX/dt (km/s) = %17.8e\n', state (4) )
fprintf( ' dY/dt (km/s) = %17.8e\n', state (5) )
fprintf( ' dZ/dt (km/s) = %17.8e\n', state (6) )
fprintf( '\n' )
fprintf( 'Ellipsoid shape parameters:\n' )
fprintf( '\n' )
fprintf( ' Equatorial radius (km) = %17.8e\n', re )
fprintf( ' Polar radius (km) = %17.8e\n', rp )
fprintf( ' Flattening coefficient = %17.8e\n', f )
fprintf( '\n' )
fprintf( 'Planetographic coordinates:\n' )
fprintf( '\n' )
fprintf( ' Longitude (deg) = %17.8e\n', ...
lon / cspice_rpd )
fprintf( ' Latitude (deg) = %17.8e\n', ...
lat / cspice_rpd )
fprintf( ' Altitude (km) = %17.8e\n', alt )
fprintf( '\n' )
fprintf( 'Planetographic velocity:\n' )
fprintf( '\n' )
fprintf( ' d Longitude/dt (deg/s) = %17.8e\n', ...
pgrvel(1)/cspice_rpd )
fprintf( ' d Latitude/dt (deg/s) = %17.8e\n', ...
pgrvel(2)/cspice_rpd )
fprintf( ' d Altitude/dt (km/s) = %17.8e\n', pgrvel(3) )
fprintf( '\n' )
fprintf( 'Rectangular coordinates from inverse mapping:\n' )
fprintf( '\n' )
fprintf( ' X (km) = %17.8e\n', rectan (1) )
fprintf( ' Y (km) = %17.8e\n', rectan (2) )
fprintf( ' Z (km) = %17.8e\n', rectan (3) )
fprintf( '\n' )
fprintf( 'Rectangular velocity from inverse mapping:\n' )
fprintf( '\n' )
fprintf( ' dX/dt (km/s) = %17.8e\n', drectn (1) )
fprintf( ' dY/dt (km/s) = %17.8e\n', drectn (2) )
fprintf( ' dZ/dt (km/s) = %17.8e\n', drectn (3) )
fprintf( '\n' )
%
% It's always good form to unload kernels after use,
% particularly in Matlab due to data persistence.
%
cspice_kclear
When this program was executed on a Mac/Intel/Octave6.x/64-bit
platform, the output was:
Rectangular coordinates:
X (km) = 1.46039732e+08
Y (km) = 2.78546607e+08
Z (km) = 1.19750315e+08
Rectangular velocity:
dX/dt (km/s) = -4.70432720e+01
dY/dt (km/s) = 9.07326134e+00
dZ/dt (km/s) = 4.75791694e+00
Ellipsoid shape parameters:
Equatorial radius (km) = 3.39619000e+03
Polar radius (km) = 3.37620000e+03
Flattening coefficient = 5.88600756e-03
Planetographic coordinates:
Longitude (deg) = 2.97667659e+02
Latitude (deg) = 2.08445040e+01
Altitude (km) = 3.36531825e+08
Planetographic velocity:
d Longitude/dt (deg/s) = -8.35770664e-06
d Latitude/dt (deg/s) = 1.59355667e-06
d Altitude/dt (km/s) = -1.12116008e+01
Rectangular coordinates from inverse mapping:
X (km) = 1.46039732e+08
Y (km) = 2.78546607e+08
Z (km) = 1.19750315e+08
Rectangular velocity from inverse mapping:
dX/dt (km/s) = -4.70432720e+01
dY/dt (km/s) = 9.07326134e+00
dZ/dt (km/s) = 4.75791694e+00
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 cspice_furnsh.
The definition of this kernel variable controls the behavior of
the CSPICE planetographic routines
cspice_pgrrec
cspice_recpgr
cspice_dpgrdr
cspice_drdpgr
It does not affect the other SPICE coordinate conversion
routines.
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 by a routine in the
call tree of this routine.
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 by a routine in the
call tree of this routine. 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 by a routine in
the call tree of this routine.
4) If the equatorial radius is non-positive, the error
SPICE(VALUEOUTOFRANGE) is signaled by a routine in the call
tree of this routine.
5) If the flattening coefficient is greater than or equal to one,
the error SPICE(VALUEOUTOFRANGE) is signaled by a routine in
the call tree of this routine.
6) If any of the input arguments, `body', `lon', `lat', `alt',
`re' or `f', is undefined, an error is signaled by the Matlab
error handling system.
7) If any of the input arguments, `body', `lon', `lat', `alt',
`re' or `f', is not of the expected type, or it does not have
the expected dimensions and size, an error is signaled by the
Mice interface.
8) If the input vectorizable arguments `lon', `lat' and `alt' do
not have the same measure of vectorization (N), an error is
signaled by the Mice interface.
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.
None.
MICE.REQ
None.
J. Diaz del Rio (ODC Space)
S.C. Krening (JPL)
E.D. Wright (JPL)
-Mice Version 1.1.0, 24-AUG-2021 (EDW) (JDR)
Added complete example to the -Examples section.
Added -Parameters, -Exceptions, -Files, -Restrictions,
-Literature_References and -Author_and_Institution sections.
Eliminated use of "lasterror" in rethrow.
Removed reference to the function's corresponding CSPICE header from
-Required_Reading section.
-Mice Version 1.0.0, 09-NOV-2012 (EDW) (SCK)
Jacobian of rectangular w.r.t. planetographic coordinates
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