:                 targetValue *= M2MM;
>                 targetUnit = Milimeter;
:                 break;
../../core/utilities/geolocation/engine/core/MarbleLocale.cpp:102: Milimeter ==> Millimeter
: 
>         case Milimeter:
:             return i18nc("means milimeters", "mm");
../../core/utilities/geolocation/engine/core/MarbleLocale.cpp:162: Milimeter ==> Millimeter
:         case Milimeter:
>             return i18nc("means milimeters", "mm");
: 
../../core/utilities/geolocation/engine/core/MarbleLocale.cpp:163: milimeters ==> millimeters
:         Kilometer,
>         Milimeter,
:         Centimeter,
../../core/utilities/geolocation/engine/core/MarbleLocale.h:56: Milimeter ==> Millimeter
: 
>     double d, td, tt, pp, ot, nt;
:     double lam, ii, omg, omb, ee;
../../core/utilities/geolocation/engine/astro/astr2lib.cpp:2007: ot ==> to, of, or, not, it
:     pp = pi2 * frac((305.0 + 10.2077 * tt) / 360.0);
>     ot = pi2 * frac((276.49 + td) / 360.0);
:     nt = pi2 * frac((44.5 - td) / 360.0);
../../core/utilities/geolocation/engine/astro/astr2lib.cpp:2019: ot ==> to, of, or, not, it
:     // osculating orbit elements
>     ee = 0.00021 * sin(pp) + 0.001 * sin(ot);
:     omg = 0.00021 * cos(pp) + 0.001 * cos(ot);
../../core/utilities/geolocation/engine/astro/astr2lib.cpp:2023: ot ==> to, of, or, not, it
:     ee = 0.00021 * sin(pp) + 0.001 * sin(ot);
>     omg = 0.00021 * cos(pp) + 0.001 * cos(ot);
:     omb = atan2(ee, omg);
../../core/utilities/geolocation/engine/astro/astr2lib.cpp:2024: ot ==> to, of, or, not, it
:     pp = pi2 * frac((356.87 - 10.2077 * tt) / 360.0);
>     ot = sin(pp);
:     lam = pi2 * frac((359.4727 + 79.69004007 * d) / 360.0);
../../core/utilities/geolocation/engine/astro/astr2lib.cpp:2039: ot ==> to, of, or, not, it
:     lam = pi2 * frac((359.4727 + 79.69004007 * d) / 360.0);
>     lam = lam + kap * sg0 * tan(0.5 * ie) * ot;
:     ii = ie - 7.9412480966E-4 + kap * sg0 * cos(pp)
../../core/utilities/geolocation/engine/astro/astr2lib.cpp:2041: ot ==> to, of, or, not, it
:     omg = oe - 1.3613568166E-4
>           + (kap * sg0 * ot + 3.5081117965E-4 * sin(nt)) / sin(ie);
: 
../../core/utilities/geolocation/engine/astro/astr2lib.cpp:2045: ot ==> to, of, or, not, it
