From aee044f652bd4a933e3aa22a17573c30684bdb11 Mon Sep 17 00:00:00 2001 From: Jonathan Bosson Date: Thu, 2 Mar 2017 16:12:55 -0700 Subject: [PATCH] exclude cache from esri --- .gitignore | 3 +- data/scene/missions/juno/juno/juno.mod | 23 ++-- data/spice/naif0011.tls | 148 +++++++++++++++++++++++++ 3 files changed, 163 insertions(+), 11 deletions(-) create mode 100644 data/spice/naif0011.tls diff --git a/.gitignore b/.gitignore index 38d00d5e83..2db24ce1fb 100644 --- a/.gitignore +++ b/.gitignore @@ -120,4 +120,5 @@ data/spice/plu055.bsp data/spice/Rosetta data/spice/sat375.bsp data/scene/lodglobes/saturn/Launcher.config -data/scene/lodglobes/mars/test_stats \ No newline at end of file +data/scene/lodglobes/mars/test_stats +data/scene/lodglobes/saturn/GDAL_cache_ESRI_Imagery_World_2d/ \ No newline at end of file diff --git a/data/scene/missions/juno/juno/juno.mod b/data/scene/missions/juno/juno/juno.mod index c9e4cc56df..12c2d45131 100644 --- a/data/scene/missions/juno/juno/juno.mod +++ b/data/scene/missions/juno/juno/juno.mod @@ -126,16 +126,19 @@ return { Name = "JunoTrail", Parent = "JupiterBarycenter", Renderable = { - Type = "RenderableTrailTrajectory", - Translation = { - Type = "SpiceTranslation", - Body = "JUNO", - Observer = "JUPITER BARYCENTER" - }, - Color = { 0.70, 0.50, 0.20 }, - StartTime = "2016 JUN 28", - EndTime = "2016 APR 01", - SampleInterval = 3600 + Type = "RenderableTrail", + Body = "JUNO", + Frame = "GALACTIC", + Observer = "JUPITER BARYCENTER", + RGB = { 0.70,0.50,0.20 }, + TropicalOrbitPeriod = 394250.0, + EarthOrbitRatio = 4.5, + DayLength = 9.9259, + TimeStamps = false, + Textures = { + Type = "simple", + Color = "textures/glare_blue.png", + }, }, }, } diff --git a/data/spice/naif0011.tls b/data/spice/naif0011.tls new file mode 100644 index 0000000000..58fcbcbd7f --- /dev/null +++ b/data/spice/naif0011.tls @@ -0,0 +1,148 @@ +KPL/LSK + + +LEAPSECONDS KERNEL FILE +=========================================================================== + +Modifications: +-------------- + +2015, Jan. 5 NJB Modified file to account for the leapsecond that + will occur on June 30, 2015. + +2012, Jan. 5 NJB Modified file to account for the leapsecond that + will occur on June 30, 2012. + +2008, Jul. 7 NJB Modified file to account for the leapsecond that + will occur on December 31, 2008. + +2005, Aug. 3 NJB Modified file to account for the leapsecond that + will occur on December 31, 2005. + +1998, Jul 17 WLT Modified file to account for the leapsecond that + will occur on December 31, 1998. + +1997, Feb 22 WLT Modified file to account for the leapsecond that + will occur on June 30, 1997. + +1995, Dec 14 KSZ Corrected date of last leapsecond from 1-1-95 + to 1-1-96. + +1995, Oct 25 WLT Modified file to account for the leapsecond that + will occur on Dec 31, 1995. + +1994, Jun 16 WLT Modified file to account for the leapsecond on + June 30, 1994. + +1993, Feb. 22 CHA Modified file to account for the leapsecond on + June 30, 1993. + +1992, Mar. 6 HAN Modified file to account for the leapsecond on + June 30, 1992. + +1990, Oct. 8 HAN Modified file to account for the leapsecond on + Dec. 31, 1990. + + +Explanation: +------------ + +The contents of this file are used by the routine DELTET to compute the +time difference + +[1] DELTA_ET = ET - UTC + +the increment to be applied to UTC to give ET. + +The difference between UTC and TAI, + +[2] DELTA_AT = TAI - UTC + +is always an integral number of seconds. The value of DELTA_AT was 10 +seconds in January 1972, and increases by one each time a leap second +is declared. Combining [1] and [2] gives + +[3] DELTA_ET = ET - (TAI - DELTA_AT) + + = (ET - TAI) + DELTA_AT + +The difference (ET - TAI) is periodic, and is given by + +[4] ET - TAI = DELTA_T_A + K sin E + +where DELTA_T_A and K are constant, and E is the eccentric anomaly of the +heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores +small-period fluctuations, is accurate to about 0.000030 seconds. + +The eccentric anomaly E is given by + +[5] E = M + EB sin M + +where M is the mean anomaly, which in turn is given by + +[6] M = M + M t + 0 1 + +where t is the number of ephemeris seconds past J2000. + +Thus, in order to compute DELTA_ET, the following items are necessary. + + DELTA_TA + K + EB + M0 + M1 + DELTA_AT after each leap second. + +The numbers, and the formulation, are taken from the following sources. + + 1) Moyer, T.D., Transformation from Proper Time on Earth to + Coordinate Time in Solar System Barycentric Space-Time Frame + of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981), + 33-56 and 57-68. + + 2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical + Reference System on Algorithms for Computing Time Differences + and Clock Rates, JPL IOM 314.5--942, 1 October 1985. + +The variable names used above are consistent with those used in the +Astronomical Almanac. + +\begindata + +DELTET/DELTA_T_A = 32.184 +DELTET/K = 1.657D-3 +DELTET/EB = 1.671D-2 +DELTET/M = ( 6.239996D0 1.99096871D-7 ) + +DELTET/DELTA_AT = ( 10, @1972-JAN-1 + 11, @1972-JUL-1 + 12, @1973-JAN-1 + 13, @1974-JAN-1 + 14, @1975-JAN-1 + 15, @1976-JAN-1 + 16, @1977-JAN-1 + 17, @1978-JAN-1 + 18, @1979-JAN-1 + 19, @1980-JAN-1 + 20, @1981-JUL-1 + 21, @1982-JUL-1 + 22, @1983-JUL-1 + 23, @1985-JUL-1 + 24, @1988-JAN-1 + 25, @1990-JAN-1 + 26, @1991-JAN-1 + 27, @1992-JUL-1 + 28, @1993-JUL-1 + 29, @1994-JUL-1 + 30, @1996-JAN-1 + 31, @1997-JUL-1 + 32, @1999-JAN-1 + 33, @2006-JAN-1 + 34, @2009-JAN-1 + 35, @2012-JUL-1 + 36, @2015-JUL-1 ) + +\begintext + +