spkw05 |
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ProcedureSPKW05 ( Write SPK segment, type 5 ) SUBROUTINE SPKW05 ( HANDLE, BODY, CENTER, FRAME, FIRST, LAST, . SEGID, GM, N, STATES, EPOCHS ) AbstractWrite an SPK segment of type 5 given a time-ordered set of discrete states and epochs, and the gravitational parameter of a central body. Required_ReadingSPK SPC NAIF_IDS KeywordsEPHEMERIS DeclarationsIMPLICIT NONE INTEGER HANDLE INTEGER BODY INTEGER CENTER CHARACTER*(*) FRAME DOUBLE PRECISION FIRST DOUBLE PRECISION LAST CHARACTER*(*) SEGID DOUBLE PRECISION GM INTEGER N DOUBLE PRECISION STATES ( 6, * ) DOUBLE PRECISION EPOCHS ( * ) Brief_I/OVARIABLE I/O DESCRIPTION -------- --- -------------------------------------------------- HANDLE I Handle of an SPK file open for writing. BODY I Body code for ephemeris object. CENTER I Body code for the center of motion of the body. FRAME I The reference frame of the states. FIRST I First valid time for which states can be computed. LAST I Last valid time for which states can be computed. SEGID I Segment identifier. GM I Gravitational parameter of central body. N I Number of states and epochs. STATES I States. EPOCHS I Epochs. Detailed_InputHANDLE is the file handle of an SPK file opened for writing. BODY is the NAIF ID for the body whose states are to be recorded in an SPK file. CENTER is the NAIF ID for the center of motion associated with BODY. FRAME is the reference frame that states are referenced to, for example 'J2000'. FIRST, LAST are the bounds on the ephemeris times, expressed as seconds past J2000, for which the states can be used to interpolate a state for BODY. SEGID is the segment identifier. An SPK segment identifier may contain up to 40 characters. GM is the gravitational parameter of the central body ( in units of kilometers **3 / seconds **2 ). N is the number of states and epochs to be stored in the segment. STATES contains a time-ordered array of geometric states ( x, y, z, dx/dt, dy/dt, dz/dt, in kilometers and kilometers per second ) of the target body with respect to the central body specified in the segment descriptor. EPOCHS contains the epochs (ephemeris seconds past J2000) corresponding to the states in STATES. Epochs must form a strictly increasing sequence. Detailed_OutputNone. A type 5 segment is written to the file attached to HANDLE. ParametersNone. Exceptions1) If GM is not positive, the error SPICE(NONPOSITIVEMASS) is signaled. 2) If the input epochs do not form an increasing sequence, the error SPICE(UNORDEREDTIMES) is signaled. 3) If the number of states and epochs is not positive, the error SPICE(NUMSTATESNOTPOS) is signaled. 4) If FIRST is greater than LAST, the error SPICE(BADDESCRTIMES) is signaled. 5) If SEGID is more than 40 characters long, the error SPICE(SEGIDTOOLONG) is signaled. 6) If SEGID contains any nonprintable characters, the error SPICE(NONPRINTABLECHARS) is signaled. 7) If a file I/O problem occurs, an error is signaled by a routine in the call tree of this routine. FilesA new type 05 SPK segment is written to the SPK file attached to HANDLE. ParticularsThis routine writes an SPK type 05 data segment to the open SPK file according to the format described in the type 05 section of the SPK Required Reading. The SPK file must have been opened with write access. ExamplesThe 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) This example demonstrates how to create an SPK type 5 kernel containing only one segment, given a time-ordered set of discrete states and epochs, and the gravitational parameter of a central body. Example code begins here. PROGRAM SPKW05_EX1 IMPLICIT NONE C C Local parameters. C INTEGER NAMLEN PARAMETER ( NAMLEN = 40 ) C C Define the segment identifier parameters. C CHARACTER*(*) SPK5 PARAMETER ( SPK5 = 'spkw05_ex1.bsp' ) CHARACTER*(*) REF PARAMETER ( REF = 'J2000' ) DOUBLE PRECISION GMSUN PARAMETER ( GMSUN = 132712440023.310D0 ) INTEGER BODY PARAMETER ( BODY = 3 ) INTEGER CENTER PARAMETER ( CENTER = 10 ) INTEGER NSTATS PARAMETER ( NSTATS = 9 ) C C Local variables. C CHARACTER*(NAMLEN) IFNAME CHARACTER*(NAMLEN) SEGID DOUBLE PRECISION EPOCHS ( NSTATS ) DOUBLE PRECISION FIRST DOUBLE PRECISION LAST DOUBLE PRECISION STATES ( 6, NSTATS ) INTEGER HANDLE INTEGER NCOMCH C C Define the states and epochs. C DATA STATES / . 101.D0, 201.D0, 301.D0, 401.D0, 501.D0, 601.D0, . 102.D0, 202.D0, 302.D0, 402.D0, 502.D0, 602.D0, . 103.D0, 203.D0, 303.D0, 403.D0, 503.D0, 603.D0, . 104.D0, 204.D0, 304.D0, 404.D0, 504.D0, 604.D0, . 105.D0, 205.D0, 305.D0, 405.D0, 505.D0, 605.D0, . 106.D0, 206.D0, 306.D0, 406.D0, 506.D0, 606.D0, . 107.D0, 207.D0, 307.D0, 407.D0, 507.D0, 607.D0, . 108.D0, 208.D0, 308.D0, 408.D0, 508.D0, 608.D0, . 109.D0, 209.D0, 309.D0, 409.D0, 509.D0, 609.D0 / DATA EPOCHS / 100.D0, 200.D0, 300.D0, . 400.D0, 500.D0, 600.D0, . 700.D0, 800.D0, 900.D0 / C C Set the start and end times of interval covered by C segment. C FIRST = EPOCHS(1) LAST = EPOCHS(NSTATS) C C NCOMCH is the number of characters to reserve for the C kernel's comment area. This example doesn't write C comments, so set to zero. C NCOMCH = 0 C C Internal file name and segment ID. C IFNAME = 'Type 5 SPK internal file name.' SEGID = 'SPK type 5 test segment' C C Open a new SPK file. C CALL SPKOPN( SPK5, IFNAME, NCOMCH, HANDLE ) C C Write the segment. C CALL SPKW05 ( HANDLE, BODY, CENTER, REF, . FIRST, LAST, SEGID, GMSUN, . NSTATS, STATES, EPOCHS ) C C Close the SPK file. C CALL SPKCLS ( HANDLE ) END When this program is executed, no output is presented on screen. After run completion, a new SPK type 5 exists in the output directory. RestrictionsNone. Literature_ReferencesNone. Author_and_InstitutionJ. Diaz del Rio (ODC Space) K.R. Gehringer (JPL) J.M. Lynch (JPL) B.V. Semenov (JPL) W.L. Taber (JPL) I.M. Underwood (JPL) E.D. Wright (JPL) VersionSPICELIB Version 1.2.0, 17-JUN-2021 (JDR) Added IMPLICIT NONE statement. Edited the header to comply with NAIF standard. Added complete example code from existing fragment. Removed unnecessary $Revisions section. SPICELIB Version 1.1.0, 30-OCT-2006 (BVS) Removed restriction that the input reference frame should be inertial by changing the routine that determines the frame ID from the name from IRFNUM to NAMFRM. SPICELIB Version 1.0.2, 27-JAN-2003 (EDW) Added error check to catch non-positive gravitational parameter GM. SPICELIB Version 1.0.1, 05-OCT-1993 (KRG) Removed all references to a specific method of opening the SPK file in the $Brief_I/O, $Detailed_Input, $Particulars and $Examples sections of the header. It is assumed that a person using this routine has some knowledge of the DAF system and the methods for obtaining file handles. SPICELIB Version 1.0.0, 01-APR-1992 (JML) (WLT) (IMU) |
Fri Dec 31 18:36:55 2021