INS
GUI User’s Manual
Inertial Labs, Inc
TM
Address: 39959 Catoctin Ridge Street, Paeonian Springs, VA 20129 U.S.A.
Tel: +1 (703) 880-4222, Fax: +1 (703) 935-8377 Website: www.inertiallabs.com
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- “(Manual)” is to consider manually bases deviation angles on
corresponding angles “”, “” и “”.
Fields “Tilter” are used by the developer for internal tests of the INS. The
question on their use for external tests should be coordinated with the
developer – Inertial Labs company.
The button “Accumulate Data” (see Fig. 8.4) consistently starts INS units for
operation. Automatically, in the top part of the check accuracy window the
page “Current angle, deg” opens in which in the form of the graph the
current measured angle (Heading, Pitch or Roll) is plotted. Upon completion
of data collecting there is an averaging the measured data and switching on
a following controllable angle, and in a folder where there is file
INS_GUI.exe, the file of the report like Accuracy_*.txt is kept. It is a service
file which can be used for continuation of testing INS after any possible
failure in work. In that case for loading the previous measured data the
button “Load Data” is used.
Notes.
1. The filename Accuracy_*.txt consists of the word Accuracy_ and 8-12 numbers of
year, month, date, hour and minutes when the work was carrying out.
2. The button “Load Data” opens the standard window Windows “Open…”, in which it is
necessary to choose and download a file Accuracy_*.txt with the last measured data.
In pages “Heading, deg”, “Pitch, deg”, “Roll, deg”, “Temperature, codes” the
current same INS parameters are displayed in the form of graphs.
After the end of the accuracy test cycle the page “Angle Error, deg” is
opened automatically, where Angle is Heading, Pitch or Roll, depending on
the angle, where the test was carried out. In the page window the graph of
given angle calculation error is displayed, and the minimal and maximal
error values during the test, its root-mean-square value (RMS) are indicated.
Also standard deviation (STD) of measurement noise at last position of the
INS is displayed.
Note. Page “Current Heading, deg” changes its name on “Current Pitch, deg” or “Current
Roll, deg” and the page “Heading Error, deg” changes its name on “Pitch Error, deg” “Roll
Error, deg” depending on the chosen controlled parameter in left top corner of the
window “Accuracy” (see Fig. 8.4).