Position measurement of flight hardware components, such
as Solid Rocket Boosters, External Tank, and Shuttle Orbiter, is a critical
step in the stacking and processing flow of the Shuttle Space Transport
System. Surveyors who deal with land, construction, and highway surveying
often deal with similar position measurement problems. Even though the
surveying techniques used to locate Shuttle components and launch support
equipment make use of similar mathematical techniques (based on the fundamentals
of trigonometry and plane geometry), the instrumentation used by NASA and
United Space Alliance (USA) in these kinds of operations greatly surpasses
the measurement precision capabilities of typical surveying equipment.

Figure 1. Example Survey Results of Two Targets
A low-cost alternative to expensive laboratory-grade surveying instrumentation
was proposed and evaluated by the Engineering Development Contractor,
Dynacs Inc., at KSC. This alternative is a digital vision system,
composed of
a digital camera, computer, and flat black and white targets. Figure
1 shows an example of relative error between true target positions
and measured
positions during a test of the vision measurement system. True target
positions were determined by a precision survey performed by
the NASA and USA Optics
Group, using an array of high-quality laboratory-grade theodolites
(see figure 2). The measurement error of the NASA/USA survey
is less than 1
millimeter (mm).
In our test of the camera position measurement system, the camera
coordinate system’s origin is a point on the camera axis at a distance f in
front of the charged couple device (f is the focal length of the lens).
The z-axis is positive in front and away from the camera origin. The
x-axis is horizontal and positive to the left of the camera origin. The
y-axis
is vertical and positive up from the camera origin.
The formulas described in figure 3 estimate the camera position measurement
resolution limit. Note that the numerical values give error in
millimeters with z in feet. The x, y, z error can be larger than
that predicted
by the equations in figure 3. Lens distortion may be the primary
cause. An
example of y error, shown in figure 4, is approximately within
the theoretical error, since the target positions in this test
were all
near the y-axis,
where lens distortion has minimal effect. As shown in figure 4,
the z measurement resolution is usually much lower than the x
and y measurement
resolutions.
However, at close range (distance between camera and targets),
the z resolution can surpass the x and y resolution.
The low-cost advantage of the digital camera vision position measurement
system may offset the lower position resolution disadvantages
in many applications.
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Key accomplishments:
- Developed and
demonstrated vision system algorithms for independently locating
x, y, and z positions of multiple targets, as well as measuring the
relative distance between target pairs.
- Derived a set
of formulas, which approximates the limit of measurement precision
of a camera surveying system. These formulas relate the vision system
(camera, lens, and target) parameters to the best measurement resolution
that can be expected.

Figure 2. One of Four High-Precision Theodolites Used To Locate
True
Position of Targets
Figure 4. y Measurement Error Versus z
Figure 3. Theoretical
Measurement Limits for a 1024 x 1024 Pixel
Digital Camera
Contact:
Dr. R.C. Youngquist (Robert.Youngquist-1@ksc.nasa.gov),
YA-C3-E, (321) 867-1829
Participating Organization: Dynacs Inc. (Dr. J.E. Lane and Dr. C.D. Immer)
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