* Compute the angle between the Sun and the satellite orbit plane. * Return the angle in radians; domain +-pi/2 and with the sign of RxV.

swap two elements, as given by their indexes; no effect if either index is out of range.

add a deprecated option, that is let old_opt be equivalent to new_opt, where new_opt is the long option for one the the regular options.

add an 'ignore_off' option; this is an option '--opt' that turns off the 'ignoring of options' that was started by an 'ignore_on' option.

add an 'ignore_on' option; this is an option '--opt' that causes the options that follow to be ignored, until an 'ignore_off' option is found.

Compute the corrected range at RECEIVE time, from receiver at position Rx, to the GPS satellite given by SatID sat, as well as all the CER quantities,

get the covariance matrix

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------------------------------------------------------------- Define the text after 'Usage: '; default is '\<prgm\> [options] ...'

Evaluate the polynomial at the given time; singular * problems return zero. */

--------------------------------------------------------------------------------- Compute Greenwich Mean Sidereal Time in degrees

* @name GPSWeekZcount Basic Operations */ @{ * Default Constructor. * All elements are initialized to zero. */

Get Modified Julian Date MJD @warning For some compilers, this result may have diminished accuracy.

return maximum X value

return maximum Y value

return minimum X value

return minimum Y value

explicit constructor, no defaults

this function computes the number of valid header records which WriteHeaderRecords will write

Computes rotation about axis Z. * @param angle Angle to rotate, in degrees * @return A triple which is the original triple rotated an

A Simple Constructor.

return computed X standard deviation

Probability density function (PDF) of the Student t distribution. The null hypotheses that test the true mean, mu, against the standard or

* Default Constructor. * Reads the system clock for the current system time. */

return computed X variance

return conditional variance = (uncertainty y given x)^2

@} * @name YDSTime Basic Operations */ @{ * Default Constructor. * All elements are set to zero by default. */

------------------------------------------------------------------------------- add data at one epoch. May be repeated at the same epoch, but MUST be

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return the stats as a single string

Cleans the list of strings given as `pieces`. It replaces multiple newlines by a maximum of 2 and returns a new list. It also wraps t

Clear the contents of the (filename, header) map

Create a deep copy of this object.

Compute the composite Integrity Assured (IA) User Range Accuracy (URA) in meters * * This applies to both GPS CNav and GPS CNav-2.

returns the number of columns in this slice

returns the starting row in the base matrix of this slice

returns the number of elements between the i'th and i+1'th row

TD ? obsolete this by always using transpose when you must loop over columns private function to build a "column map" for this matrix, conta

--------------------------------------------------------------------------------- Compute the site displacement vector at the given time for the given

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--------------------------------------------------------------------------------- Compute the site displacement due to solid Earth tides for the given

======================================================================= Test for the TimeRange constructors ==========================================

Translate system enumeration to its string representation. * @note The string representation is being used in file * formats, e.g. Raw

* Bit wise copy from another PackecNavBits. * None of the meta-data (transmit time, SatID, ObsID) * will be changed. */

This is a bit of a kludge to deal with the fact that * Position doesn't store the actual ellipsoid model but * rather a couple of

--------------------------------------------------------------------------------- Corrections to Earth rotation due to zonal tides using USNO algorith

--------------------------------------------------------------------------------- Corrections to Earth rotation due to zonal tides using USNO IERS2003

datasize - number of non-zero data

set the 'small slips' limit

Convenience output method.

============================================================================= Test will check the dump method for various verbosities ================

------------------------------------------------------------------------------------ -----------------------------------------------------------------

Parses the file set in the initialization. The resulting data is stored in `self.pieces`.

get the aposteriori variance of unit weight; return zero if not enough data has been collected.

Compute alpha (also called gamma) = (beta^2-1) = * ((fa/fb)^2-1) for 2 frequencies fa,fb for the given satellite * system (sat.id is ign

Compute beta(a,b), the ratio of 2 frequencies fb/fa for the * given satellite system. * @return 0 if either of the input n's are not val

access the clock bias, in second