Download our Free Trial package to see if Beam Four is right for you!
Our Demo Version is fully functional on input, computational procedures, and graphical display, lacking only the file output functions of the full product.
Download Free Trial!
HOW TO SET UP AN AUXILIARY OPTICAL AXIS
(c) 1992, 2003, 2009 M.Lampton
STELLAR SOFTWARE
Suppose a group of optical elements is to be lined up along
some axis that is neither the lab X, Y, or Z directions. How
does one express the positions and orientations of its elements
in the lab frame to enter them into a BEAM optics table?
This auxiliary axis will have its origin somewhere in space,
say (Xa Ya Za). It will also have some direction along which
the optical elements are aligned. There are three ways to set
up the auxiliary axis, depending on what you initially know
about its direction:
A: the angles (tilt, pitch) of its normal are known. Tilt is
the rotation of a surface about the lab X axis; pitch is the
rotation about the tilted Y axis.
B: its direction cosines (U, V, W) are known. These are
the projections of a unit vector along the auxiliary axis
onto the lab X,Y,Z directions.
C: a second point (Xf Yf Zf) along the axis is known.
CASE A: The pitch and tilt numbers are used by BEAM to
orient the optical components so that they are normal to the
auxiliary axis. Put these into your optics table in your pitch
and tilt columns. Compute U,V,W using the formulas
U = sin(pitch)
V = -sin(tilt) * cos(pitch)
W = cos(tilt) * cos(pitch)
and then position each element using its known distance D from the
origin of the auxiliary axis (a spreadsheet is useful here):
(X0+U*D1, Y0+V*D1, Z0+W*D1) for the first element
(X0+U*D2, Y0+V*D2, Z0+W*D2) for the second element
(X0+U*D3, Y0+V*D3, Z0+W*D3) for the third element
(X0+U*D4, Y0+V*D4, Z0+W*D4) etc.
CASE B: First find the pitch and tilt of all the auxiliary
elements, using the formulas
pitch = arcsin(U)
tilt = arctan(-V/W).
Put these values, in degrees, into your optics table under
pitch and tilt column headers. Copy these numbers down the
page so that they apply to all the elements that are aligned on
your auxiliary axis. Then position each element along the
auxiliary axis using the position formulas in case A.
CASE C: First find the direction cosines of your auxiliary
axis using the Pythagorean theorem:
D = sqrt((Xf-Xa)^2 + (Yf-Ya)^2 + (Zf-Za)^2)
U = (Xf-Xa)/D
V = (Yf-Ya)/D
W = (Zf-Za)/D.
Then, with these numbers known, go to case B and complete the
pitch, tilt, and element positioning.