Ground based telescopes
have two main types of mounts. One is
the hour angle declination mount, which has
its axes lining up with the axes of right
ascension and declination. This means
that its axes are in reference with the
celestial sphere. This mount is
preferred because once the declination is
set no more adjusts need to be made along
that direction, and compensation for right
ascension can be handled with a simple hour
angle timing device. The other type of
mount is the azimuth-elevation mount.
This mount has its reference points at the
local horizon and due North. Azimuth
is rotational motion from North along the
horizontal plane, while elevation is the
motion from the horizon along a vertical
plane. The azimuth-elevation mount
must always track the apparent motion of
stars in both planes, even once they are
locked on. This, of course, is not as
easy as with the hour angle declination
mount which must only move one axis to
compensate for the earth's rotation.
However, large and heavy telescopes are
usually based on the azimuth-elevation mount
because of the simpler, less costly
structural requirements.
The SOFIA is a unique hybrid of the
azimuth-elevation mount and a spherical
bearing, since it is not a ground-based
observatory but a stratospheric observatory.
The airplane
itself provides a coarse rotating platform
for the azimuth axis (directional heading
and yaw) and the telescope bulkhead
suspension provides limited coarse rotation
(from 20 to 60 degrees) for the elevation
axis. The SOFIA
telescope is precisely moved (within +/-
3 degrees) on a large, low friction
spherical bearing, which is controlled in
three dimensions. These three perpendicular
directions are called the line-of-sight
(LOS), elevation, (Figure
1) and cross-elevation (Figure
2). The telescope cross-elevation is not
along the horizontal azimuth plane, since it
is elevated at some angle above the plane's
horizontal. The pointing direction of
cross-elevation, together with the elevation
and the aircraft heading and yaw is
difficult to visualize, but it can be
precisely converted with trigonometric
transformation:
true-azimuth(deg)
= heading - 90 + yaw +
cross-elevation*cosine(elevation)
Likewise the true
elevation must include a correction for
aircraft roll. The azimuth-elevation can, in
turn, be converted to hour-angle-declination
coordinates for a standard portable
telescope according to the latitude of the
aircraft; figure 3
gives an example of the relations for
35-degree north latitude. The spherical
mount, together with a stable inertial
reference, allows decoupling of the
telescope motion from the incidental motions
of the aircraft to provide precise pointing
and is what makes SOFIA unique. The total
observation area in the night at any one
moment is less than a good Earth-based
telescope because elevation angles are
limited to between 20 degrees and 60
degrees, but because of the aircraft
platform, if one selects the correct
latitude and time, all areas of the
celestial sphere can be observed.
A ground-based
telescope using an azimuth-elevation mount
can also have three axes of rotation called
line of sight (LOS), elevation, and azimuth,
which correspond to the normal x, y, and
z-axes. A telescope can rotate about
all three of these axes. These axes
and rotation about them are all
perpendicular to each other . To help
you understand the value of the third
axis think about target shooting. To
hit the target you must have the proper
elevation and azimuth. These rotations
are obviously perpendicular. Now,
imagine rotating 180 degrees about the
LOS. If your azimuth and elevation are
correct the LOS rotation will have no effect
on hitting the target, even though your view
is now upside down. Now imagine a more
general target , like a flock of geese, and
that you would like to shoot a picture of
them, centered on the lead goose. If
the geese were flying along a path which
appeared diagonal to the horizon, you would
rotate the camera along the LOS in order to
take a rational picture. Similarly,
Astronomers who are imaging object clusters
may want to rotate the LOS to compare images
taken on different nights and at different
hour angles.
SOFIA Observations
Require more than Meets the Eye
We must
remember the fact that SOFIA is an airborne
observatory and this makes targeting a star
in the SOFIA a unique experience. Many
factors must be considered together to
provide precise targeting: Earth's
rotational velocity (the date and time),
velocity of the aircraft, pitch & yaw of
the aircraft, longitudinal and latitudinal
coordinates of the aircraft. Ground based
telescopes only adjust for date and time,
with fixed translations for location, to
compute a star position. However, the SOFIA
flight must account for all these other
factors.
To perform
astronomy while in flight, a number of
systems must work together to provide a
stable observation platform. Several
subsystems are involved in this process.
They include: the aircraft autopilot, the
vibration isolation system, the spherical
air bearing, the gyro-stabilization system,
and the video star tracker. For an example
of how the autopilot contributes, imagine
the continuous calculation which must be
made for the direction and speed of the
aircraft; if SOFIA is flying west to east
over the equator at its cruising speed of
598 miles per hour its actual speed with
reference to the stars is 1635 miles per
hour because of Earth's rotational velocity
is in the same direction. On the other hand,
if the plane flies west bound then its
reference speed is 439 miles per hour. The
latitude of SOFIA also must be included,
because the Earth's surface rotational speed
is effected by changes in latitude. For
example, a plane flying west bound at the
equator is cruising at 439 mph relative to
the stars, but if it is flying over San
Francisco, where the surface rotation is
only 0.8 of that at the equator, the
cruising speed relative to the stars would
be only 232 mph. The telescope tracking a
star while on the low friction spherical
bearing doesn't change its attitude, but to
keep that attitude within the +/- 3 degrees
of allowed motion relative to the aircraft,
the elevation mount and azimuth (aircraft
heading) must be adjusted to compensate for
the local motion of the Earth, as it
rotates. Thus to properly operate
SOFIA requires many complex measurements and
calculations - "more than meets
the eye". The experiments
described at this site should help to
understand balancing the telescope and how
to use the star tracker to control its
pointing direction.