dvsep |
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ProcedureDVSEP ( Derivative of separation angle ) DOUBLE PRECISION FUNCTION DVSEP ( S1, S2 ) AbstractCalculate the time derivative of the separation angle between two input states, S1 and S2. Required_ReadingNone. KeywordsDERIVATIVES GEOMETRY DeclarationsIMPLICIT NONE DOUBLE PRECISION S1 (6) DOUBLE PRECISION S2 (6) Brief_I/OVARIABLE 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_InputS1, 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_OutputThe function returns the double precision value of the time derivative of the angular separation between S1 and S2. ParametersNone. Exceptions1) 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. FilesNone. ParticularsIn 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.) 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) 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 RestrictionsNone. Literature_ReferencesNone. Author_and_InstitutionJ. Diaz del Rio (ODC Space) E.D. Wright (JPL) VersionSPICELIB 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