partof |
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ProcedurePARTOF ( Parabolic time of flight ) SUBROUTINE PARTOF ( MA, D ) AbstractSolve the time of flight equation MA = D + (D**3) / 3 for the parabolic eccentric anomaly D, given mean anomaly. Required_ReadingNone. KeywordsCONIC DeclarationsIMPLICIT NONE DOUBLE PRECISION MA DOUBLE PRECISION D Brief_I/OVARIABLE I/O DESCRIPTION -------- --- -------------------------------------------------- MA I Mean anomaly at epoch. D O Parabolic eccentric anomaly. Detailed_InputMA is the parabolic mean anomaly of an orbiting body at some epoch t, 3 1/2 MA = (t-T) (mu/(2q )) where T is the time of periapsis passage, mu is the gravitational parameter of the primary body, and q is the perifocal distance. Detailed_OutputD is the corresponding parabolic anomaly. This is the solution to the time of flight equation 3 MA = D + D / 3 ParametersNone. ExceptionsError free. FilesNone. ParticularsIterate to solve 3 f(D,MA,p) = D + D / 3 - MA = 0 ExamplesELLTOF, HYPTOF, and PARTOF are used by CONICS. RestrictionsNone. Literature_References[1] R. Bate, D. Mueller, and J. White, "Fundamentals of Astrodynamics," Dover Publications Inc., 1971. Author_and_InstitutionJ. Diaz del Rio (ODC Space) W.L. Taber (JPL) I.M. Underwood (JPL) VersionSPICELIB Version 2.1.0, 14-APR-2021 (JDR) Added IMPLICIT NONE statement. Edited the header to comply with NAIF standard. Removed unnecessary $Revisions section. SPICELIB Version 2.0.1, 10-MAR-1992 (WLT) Comment section for permuted index source lines was added following the header. SPICELIB Version 2.0.0, 19-APR-1991 (WLT) A write statement left over from debugging days was removed. SPICELIB Version 1.0.0, 31-JAN-1990 (IMU) |
Fri Dec 31 18:36:37 2021