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pl_cache.cpp
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/* pl_cache.cpp: computes and caches planetary positions
SEE PL_CACHE.TXT FOR A DISCUSSION OF WHAT THIS DOES. It probably
won't make much sense to you if you don't.
Copyright (C) 2010, Project Pluto
This program is free software; you can redistribute it and/or
modify it under the terms of the GNU General Public License
as published by the Free Software Foundation; either version 2
of the License, or (at your option) any later version.
This program is distributed in the hope that it will be useful,
but WITHOUT ANY WARRANTY; without even the implied warranty of
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
GNU General Public License for more details.
You should have received a copy of the GNU General Public License
along with this program; if not, write to the Free Software
Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston, MA
02110-1301, USA. */
// #define TIMING_ON 1
#include <stdio.h>
#include <stdlib.h>
#include <stdint.h>
#include <string.h>
#include <assert.h>
#include <math.h>
#ifdef TIMING_ON
#include <time.h>
#endif
#include "pl_cache.h"
#include "watdefs.h"
#include "lunar.h"
#include "afuncs.h"
#include "jpleph.h"
const char *get_environment_ptr( const char *env_ptr); /* mpc_obs.cpp */
int debug_printf( const char *format, ...) /* runge.cpp */
#ifdef __GNUC__
__attribute__ (( format( printf, 1, 2)))
#endif
;
extern int debug_level;
int64_t planet_ns;
#define J2000 2451545.0
#define J0 (J2000 - 2000. * 365.25)
FILE *fopen_ext( const char *filename, const char *permits); /* miscell.cpp */
void make_config_dir_name( char *oname, const char *iname); /* miscell.cpp */
char *fgets_trimmed( char *buff, size_t max_bytes, FILE *ifile); /*elem_out.c*/
int generic_message_box( const char *message, const char *box_type);
int compute_rough_planet_loc( const double t_cen, const int planet_idx,
double *vect); /* sm_vsop.cpp */
int asteroid_position_raw( const int astnum, const double jd,
double *posn); /* bc405.cpp */
int64_t nanoseconds_since_1970( void); /* mpc_obs.c */
int format_jpl_ephemeris_info( char *buff); /* pl_cache.c */
static int planet_posn_raw( int planet_no, const double jd,
double *vect_2000)
{
static void *ps_1996_data[10];
const int jpl_center = 11; /* default to heliocentric */
int i, rval = 0;
static const char *jpl_filename = NULL;
static void *jpl_eph = NULL;
const int bc405_start = 100;
const int calc_vel = (planet_no & PLANET_POSN_VELOCITY_FLAG) ? 1 : 0;
planet_no &= ~PLANET_POSN_VELOCITY_FLAG;
if( !planet_no) /* the sun */
{
vect_2000[0] = vect_2000[1] = vect_2000[2] = 0.;
if( !jd && jpl_eph) /* return version data: */
{
vect_2000[0] = (double)jpl_get_long( jpl_eph, JPL_EPHEM_EPHEMERIS_VERSION);
vect_2000[1] = jpl_get_double( jpl_eph, JPL_EPHEM_START_JD);
vect_2000[2] = jpl_get_double( jpl_eph, JPL_EPHEM_END_JD);
}
return( 0);
}
if( planet_no >= bc405_start && planet_no < bc405_start + 300)
{
double temp_loc[4];
rval = asteroid_position_raw( planet_no - bc405_start, jd, temp_loc);
if( debug_level > 8)
debug_printf( "JD %f, minor planet %d: (%f %f %f)\n",
jd, planet_no, temp_loc[0], temp_loc[1], temp_loc[2]);
memcpy( vect_2000, temp_loc, 3 * sizeof( double));
return( rval);
}
if( !jpl_filename)
{
FILE *ifile;
#if defined (_WIN32) || defined( __WATCOMC__)
jpl_filename = get_environment_ptr( "JPL_FILENAME");
#else
jpl_filename = get_environment_ptr( "LINUX_JPL_FILENAME");
#endif
if( *jpl_filename)
jpl_eph = jpl_init_ephemeris( jpl_filename, NULL, NULL);
if( !jpl_eph)
if( (ifile = fopen_ext( "jpl_eph.txt", "fcrb")) != NULL)
{
char buff[100];
while( !jpl_eph && fgets_trimmed( buff, sizeof( buff), ifile))
if( *buff && *buff != ';')
{
jpl_eph = jpl_init_ephemeris( buff, NULL, NULL);
if( !jpl_eph)
{
char tname[255];
make_config_dir_name( tname, buff);
jpl_eph = jpl_init_ephemeris( tname, NULL, NULL);
}
}
if( debug_level)
debug_printf( "Ephemeris file %s\n", buff);
fclose( ifile);
}
if( debug_level && jpl_eph)
{
debug_printf( "\nEphemeris time span years %.3f to %.3f\n",
(jpl_get_double( jpl_eph, JPL_EPHEM_START_JD) - J0) / 365.25,
(jpl_get_double( jpl_eph, JPL_EPHEM_END_JD) - J0) / 365.25);
debug_printf( "Ephemeris version %ld\n", jpl_get_long( jpl_eph, JPL_EPHEM_EPHEMERIS_VERSION));
debug_printf( "Kernel size %ld, record size %ld, swap_bytes %ld\n",
jpl_get_long( jpl_eph, JPL_EPHEM_KERNEL_SIZE),
jpl_get_long( jpl_eph, JPL_EPHEM_KERNEL_RECORD_SIZE),
jpl_get_long( jpl_eph, JPL_EPHEM_KERNEL_SWAP_BYTES));
debug_printf( "ncon = %ld AU=%f emrat = %f\n",
jpl_get_long( jpl_eph, JPL_EPHEM_N_CONSTANTS),
jpl_get_double( jpl_eph, JPL_EPHEM_AU_IN_KM),
jpl_get_double( jpl_eph, JPL_EPHEM_EARTH_MOON_RATIO));
}
}
if( jpl_eph)
{
double state[6]; /* DE gives both posn & velocity */
int failure_code;
if( planet_no < 0) /* flag to unload everything */
{
jpl_close_ephemeris( jpl_eph);
jpl_eph = NULL;
jpl_filename = NULL;
return( 0);
}
else if( planet_no == 10)
failure_code = jpl_pleph( jpl_eph, jd, 10, 3, state, calc_vel);
else
failure_code = jpl_pleph( jpl_eph, jd,
(planet_no == 3) ? 13 : planet_no, jpl_center, state, calc_vel);
if( !failure_code) /* we're done */
{
if( debug_level > 8)
debug_printf( "JD %f, planet %d: (%f %f %f)\n",
jd, planet_no, state[0], state[1], state[2]);
equatorial_to_ecliptic( state);
memcpy( vect_2000, state + calc_vel, 3 * sizeof( double));
return( 0);
}
else
if( debug_level)
debug_printf( "Failed: JD %f, planet %d, code %d\n",
jd, planet_no, failure_code);
}
if( planet_no == 10) /* the moon */
{
double tloc[4];
if( !compute_elp_xyz( NULL, (jd - J2000) / 36525., 0., tloc))
for( i = 0; i < 3; i++)
vect_2000[i] = tloc[i] / AU_IN_KM;
else
{
static int first_time = 1;
rval = -3;
if( first_time)
generic_message_box( "\
The file 'elp82.dat' is missing. Without\n\
this file, lunar positions will be very inaccurate\n\
and orbits will be somewhat less accurate. Either\n\
get the file, or set up JPL ephemerides. See\n\
https://www.projectpluto.com/find_orb.htm#de_eph\n\
for details on how to do this.", "o");
first_time = 0;
compute_rough_planet_loc( (jd - J2000) / 36525., 10, vect_2000);
}
return( rval);
}
if( planet_no < 0) /* flag to unload everything */
{
for( i = 0; i < 10; i++)
if( ps_1996_data[i])
{
unload_ps1996_series( ps_1996_data[i]);
ps_1996_data[i] = NULL;
}
return( 0);
}
if( !ps_1996_data[planet_no])
ps_1996_data[planet_no] = load_ps1996_series( NULL, jd, planet_no);
if( !ps_1996_data[planet_no])
rval = -1;
else if( get_ps1996_position( jd, ps_1996_data[planet_no], vect_2000, 0))
{
unload_ps1996_series( ps_1996_data[planet_no]);
ps_1996_data[planet_no] = load_ps1996_series( NULL, jd, planet_no);
if( !ps_1996_data[planet_no])
rval = -2;
else if( get_ps1996_position( jd, ps_1996_data[planet_no], vect_2000, 0))
rval = -3;
}
if( !rval)
equatorial_to_ecliptic( vect_2000);
else
{
static int first_time = 1;
if( first_time)
{
generic_message_box( "\
The file 'ps_1996.dat' is missing. Without it,\n\
planetary positions will be of low accuracy. Either\n\
get the file, or set up JPL ephemerides. See\n\
https://www.projectpluto.com/find_orb.htm#de_eph\n\
for details on how to do this.", "o");
debug_printf( "Loading ps_1996: rval %d, planet %d, JD %f\n",
rval, planet_no, jd);
}
first_time = 0;
if( planet_no > 0 && planet_no < 9)
compute_rough_planet_loc( (jd - J2000) / 36525., planet_no, vect_2000);
}
return( rval);
}
#define POSN_CACHE struct posn_cache
POSN_CACHE
{
double jd;
double vect[3];
int planet_no;
};
#define POSN_NODE struct posn_node
POSN_NODE
{
double min_jd;
int used;
POSN_CACHE *data;
};
#define node_size 1659
/* When a node is 90% full, it's time to split it. */
#define splitting_size (node_size - (node_size / 10))
/* If a node reaches splitting_size, "spill over" to an adjacent */
/* node if it's less than half full : */
#define spillover_size (node_size / 2)
int n_posns_cached = 0;
/* Hash the JD and planet number. It seems a fair bit of time is
spent in this function, so I spent a good bit of time trying to make
it as simple/fast as possible while still giving good distribution
(i.e., no more or not many more table collisions than would be
expected with a "perfectly randomizing" hash function.) It helps
that node_size is not a power of two.
Note that it works well _for the planet positions being hashed
here_. Don't rely on it as a general-purpose hashing function!
Updated 2015 Feb 12: MSVC objected to simply setting
const int32_t *dword_ptr = (int32_t *)&jd;
and accessing the four-byte halves of jd directly, so we're now
doing a totally pointless memcpy. */
static inline int hash_function( const int planet_no, const double jd)
{
int32_t dword_ptr[2];
int rval;
memcpy( dword_ptr, &jd, sizeof( double));
rval = dword_ptr[0] ^ dword_ptr[1] ^ (planet_no << 8);
rval &= 0x7fffffff;
rval %= node_size;
assert( rval >= 0);
assert( rval < node_size);
return( rval);
}
/* When a node gets to 'splitting_size' values, we compact them
(removing unused entries), then partition them in half. We do
that partitioning, at least for the nonce, the lazy way : we
Shell-sort the entire array. */
static void collapse_and_partition( POSN_CACHE *ovals, const POSN_CACHE *ivals)
{
int i, j, array_size, gap_size = 1;
for( i = array_size = 0; i < node_size; i++)
if( ivals[i].planet_no)
ovals[array_size++] = ivals[i];
assert( array_size == splitting_size);
while( gap_size < array_size)
gap_size = gap_size * 3 + 1;
while( gap_size)
{
for( i = 0; i < gap_size; i++)
for( j = i; j + gap_size < array_size; )
if( ovals[j].jd > ovals[j + gap_size].jd)
{
const POSN_CACHE temp = ovals[j];
ovals[j] = ovals[j + gap_size];
ovals[j + gap_size] = temp;
if( j >= gap_size)
j -= gap_size;
}
else
j += gap_size;
gap_size /= 3;
}
}
/* The following three long ints keep track of the number of searches
and probes done, and the "worst-case" maximum number of probes required,
just to check that the hash function is truly random enough. */
// #define TEST_PLANET_CACHING_HASH_FUNCTION
#ifdef TEST_PLANET_CACHING_HASH_FUNCTION
long total_n_searches = 0, total_n_probes = 0, max_probes_required = 0;
#endif
static int find_within_node( const int planet_no, const double jd, const POSN_CACHE *cache)
{
int loc = hash_function( planet_no, jd);
int n_probes = 1;
while( cache[loc].planet_no)
{
if( cache[loc].planet_no == planet_no && cache[loc].jd == jd)
break;
n_probes++;
loc = (loc + n_probes) % node_size;
}
#if 0
for( int i = 0; i < node_size; i++)
if( i != loc)
assert( cache[i].planet_no != planet_no || cache[i].jd != jd);
#endif
#ifdef TEST_PLANET_CACHING_HASH_FUNCTION
if( max_probes_required < n_probes)
max_probes_required = n_probes;
total_n_searches++;
total_n_probes += n_probes;
#endif
return( loc);
}
/* At one time or another, I've had concerns that the scheme for caching
planetary positions (essentially a single-level hashed B-tree; see
'pl_cache.txt' for details) was buggy. The check_integrity() function does
some basic consistency tests (are all the nodes within the time range
they're supposed to be? is the number of used nodes what it's supposed to
be?) If such concerns recur, we can #define CHECK_CACHING_INTEGRITY
and see if it finds anything we need to worry about.
#define CHECK_CACHING_INTEGRITY
*/
#ifdef CHECK_CACHING_INTEGRITY
static void check_integrity( const POSN_NODE *nodes, const int n_nodes)
{
int i;
for( i = 0; i < n_nodes; i++, nodes++)
{
int j, n_used = 0;
const double max_jd = (i < n_nodes - 1 ? nodes[1].min_jd : 1e+20);
const POSN_CACHE *cptr = nodes->data;
for( j = 0; j < node_size; j++, cptr++)
if( cptr->planet_no)
{
assert( cptr->jd >= nodes->min_jd);
assert( cptr->jd <= max_jd);
n_used++;
}
assert( n_used == nodes->used);
}
}
#endif /* #ifdef CHECK_CACHING_INTEGRITY */
/* Computing planetary positions is somewhat expensive if we're using
JPL ephemerides, and _very_ expensive if we aren't (the PS-1996 method
is used, which involves lots of trig series). And frequently, we'll be
requesting the same data over and over (for example, if we're integrating
over a particular time span repeatedly). So it makes sense to cache the
planetary positions.
Below, this is done with a hash table in a very standard sort of way.
The planet_no and jd are hashed, we look in the 'cache' table, we do a
quadratic search if there's an hash collision. If we find the data, we
return it. If we don't find it, we call the planet_posn_raw( ) (uncached)
function, and add the result to the cache, and _then_ return it.
When the table is more than 80% full, we double the table size, dump
everything computed to date, and start from scratch. This is admittedly
mildly wasteful, but I don't think the performance benefit of expanding
the cache and adding everything we've got back in would be worthwhile.
(It wouldn't be hard to do, though.)
If the cache gets above some limit (currently set to a million cached
positions, or about 36 MBytes), we stop growing the cache. So if you
had a _really_ long integration, the cache gets dumped, rebuilt to the
same size, dumped again, built to the same size, etc.
Previously, the data was stored using a balanced tree. I don't know
what possessed me to do something that dumb. (At the very least, had
I keyed the tree using the above hash function, entries to the tree would
have been nearly random, and a plain old unbalanced tree would have worked
Just Fine.) */
#define MAX_N_NODES 10000
int planet_posn( const int planet_no, const double jd, double *vect_2000)
{
static POSN_NODE *nodes = NULL;
static int n_nodes = 0, n_nodes_alloced = 0, curr_node = 0;
int loc, rval = 0;
#ifdef TIMING_ON
int64_t t_start;
#endif
POSN_CACHE *cache;
assert( fabs( jd) < 1e+9);
if( !planet_no) /* the sun */
{
vect_2000[0] = vect_2000[1] = vect_2000[2] = 0.;
return( 0);
}
if( planet_no < 0 || n_nodes >= MAX_N_NODES)
{ /* flag to unload everything */
int i;
for( i = 0; i < n_nodes; i++)
if( nodes[i].data)
free( nodes[i].data);
if( nodes)
free( nodes);
nodes = NULL;
n_posns_cached = 0;
n_nodes = n_nodes_alloced = curr_node = 0;
}
if( planet_no < 0)
{
planet_posn_raw( -1, 0., NULL);
return( 0);
}
if( planet_no == PLANET_POSN_EARTH || planet_no == PLANET_POSN_MOON)
{
double moon_loc[3];
rval = planet_posn( 3, jd, vect_2000); /* first, get Earth-Moon */
if( !rval) /* barycenter posn, then */
rval = planet_posn( 10, jd, moon_loc); /* lunar offset vect */
if( !rval)
{
unsigned i;
const double EARTH_MOON_BARYCENTER_FACTOR = 82.300679;
const double factor = (planet_no == PLANET_POSN_EARTH ?
-1. / EARTH_MOON_BARYCENTER_FACTOR :
1. - 1. / EARTH_MOON_BARYCENTER_FACTOR);
for( i = 0; i < 3; i++)
vect_2000[i] += moon_loc[i] * factor;
}
return( rval);
}
if( !nodes || n_nodes == n_nodes_alloced - 1)
{
const unsigned new_n_alloced = 100 + 3 * n_nodes_alloced / 2;
nodes = (POSN_NODE *)realloc( nodes, new_n_alloced * sizeof( POSN_NODE));
assert( nodes);
if( !n_nodes_alloced) /* set up first node : */
{
n_nodes = 1;
nodes[0].min_jd = -1e+10;
nodes[0].used = 0;
nodes[0].data = (POSN_CACHE *)calloc( node_size, sizeof( POSN_CACHE));
}
n_nodes_alloced = new_n_alloced;
}
/* Now, find the right node in which to find/store this posn: */
while( curr_node + 1 < n_nodes && nodes[curr_node + 1].min_jd <= jd)
curr_node++;
while( curr_node && jd < nodes[curr_node].min_jd)
curr_node--;
assert( jd >= nodes[curr_node].min_jd);
assert( curr_node == n_nodes - 1 || jd < nodes[curr_node + 1].min_jd);
cache = nodes[curr_node].data;
loc = find_within_node( planet_no, jd, cache);
#ifdef TIMING_ON
t_start = nanoseconds_since_1970( );
#endif
if( !cache[loc].planet_no)
{
cache[loc].planet_no = planet_no;
cache[loc].jd = jd;
nodes[curr_node].used++;
rval = planet_posn_raw( planet_no, jd, cache[loc].vect);
n_posns_cached++;
}
else
{
assert( cache[loc].planet_no == planet_no);
assert( cache[loc].jd == jd);
memcpy( vect_2000, cache[loc].vect, 3 * sizeof( double));
return( rval);
}
#ifdef TIMING_ON
planet_ns += nanoseconds_since_1970( ) - t_start;
#endif
memcpy( vect_2000, cache[loc].vect, 3 * sizeof( double));
assert( nodes[curr_node].used <= splitting_size);
#ifdef CHECK_CACHING_INTEGRITY
if( n_posns_cached % 10000 == 0)
check_integrity( nodes, n_nodes);
#endif
if( nodes[curr_node].used == splitting_size)
{
POSN_CACHE *tcache = (POSN_CACHE *)calloc( node_size, sizeof( POSN_CACHE));
int i, size1 = splitting_size / 2;
const int size_left = (curr_node ? nodes[curr_node - 1].used : node_size);
const int size_right = (curr_node < n_nodes - 1 ? nodes[curr_node + 1].used : node_size);
#ifdef CHECK_CACHING_INTEGRITY
check_integrity( nodes, n_nodes);
#endif
collapse_and_partition( tcache, cache);
memset( cache, 0, node_size * sizeof( POSN_CACHE));
nodes[curr_node].used = 0;
if( size_left < size_right && size_left < spillover_size)
{ /* "spill over" to left */
curr_node--;
size1 -= size_left / 2;
if( debug_level > 5)
debug_printf( "Spilling %d to left: %d\n", curr_node, size1);
}
else if( size_right <= size_left && size_right < spillover_size)
{ /* "spill over" to right */
size1 += size_right / 2;
if( debug_level > 5)
debug_printf( "Spilling %d to right: %d\n", curr_node, size1);
}
else /* create new node */
{
memmove( nodes + curr_node + 2, nodes + curr_node + 1,
(n_nodes - curr_node - 1) * sizeof( POSN_NODE));
nodes[curr_node + 1].data = (POSN_CACHE *)calloc( node_size, sizeof( POSN_CACHE));
nodes[curr_node + 1].used = 0;
if( debug_level > 5)
debug_printf( "Splitting node %d\n", curr_node);
n_nodes++;
}
while( tcache[size1].jd == tcache[size1 - 1].jd)
size1--;
for( i = 0; i < splitting_size; i++)
{
const int n = curr_node + (i < size1 ? 0 : 1);
POSN_CACHE *cptr = nodes[n].data;
const int new_loc = find_within_node( tcache[i].planet_no,
tcache[i].jd, cptr);
cptr[new_loc] = tcache[i];
nodes[n].used++;
}
nodes[curr_node + 1].min_jd = tcache[size1].jd;
#ifdef CHECK_CACHING_INTEGRITY
check_integrity( nodes, n_nodes);
#endif
free( tcache);
}
return( rval);
}
/* In the following, we get the earth's position for a particular */
/* instant, just to ensure that JPL ephemerides (if any) are loaded. */
/* Then we call with planet = JD = 0, which causes the info about */
/* the JPL ephemerides to be put into the 'state vector'. */
int get_jpl_ephemeris_info( int *de_version, double *jd_start, double *jd_end)
{
double vect_2000[3];
planet_posn_raw( 3, J2000, vect_2000);
planet_posn_raw( 0, 0., vect_2000);
*de_version = (int)vect_2000[0];
if( jd_start)
*jd_start = (int)vect_2000[1];
if( jd_end)
*jd_end = (int)vect_2000[2];
return( 0);
}
int format_jpl_ephemeris_info( char *buff)
{
int de_version;
double jd_start, jd_end;
get_jpl_ephemeris_info( &de_version, &jd_start, &jd_end);
if( !de_version && !jd_start && !jd_end)
{
strcpy( buff, "\nNo JPL DE ephemeris file loaded; using (slower) PS1996 series\n");
strcat( buff, "See https://www.projectpluto.com/find_orb.htm#de_eph for\n");
strcat( buff, "info on how/why to use JPL DE ephemerides\n");
}
else
sprintf( buff,
"\nUsing DE-%d; covers years %.1f to %.1f\n", de_version,
(jd_start - J2000) / 365.25 + 2000.,
(jd_end - J2000) / 365.25 + 2000.);
/* Kludge to allow re-use of 'version' string */
/* between 'about' and 'main' dialogues: */
return( de_version);
}