Total In-Flight Simulator 50th Anniversary
AFRL's Total In-Flight Simulator is celebrating 50 years of service.
AFRL's Total In-Flight Simulator
(TIFS), a Convair C-131 Samaritan
aircraft, entered service on March 22,
1955. The C-131 aircraft had performed
various transport operations for
approximately a decade up to that
point, and the Air Force (AF) Flight
Dynamics Laboratory--now AFRL--
subsequently chose it for a very special
mission: developing next-generation air
vehicles.
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| Figure 1. TIFS simulation cockpit configuration |
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| Figure 2. TIFS ASTTA configuration |
Performing extensive modification,
AFRL transformed the airplane into
TIFS,
a one-of-a-kind simulator that
engineers can program to simulate
virtually any type of air vehicle, in flight,
with six degrees of freedom. When
most other C-131s left the AF's active
fleet in the late 1970s, TIFS was just
beginning to support programs such as
the space shuttle, B-1 and B-2 bombers,
and numerous private sector tests and
development efforts.
AFRL owns TIFS, and Calspan
Corporation operates it through a
Cooperative Research and Development
Agreement. Mr. Norman Weingarten,
Calspan's in-flight simulation operations
manager, began his involvement with
this airplane while working as a project
engineer during the extensive modification
effort that produced TIFS. "It's
more realistic than a ground simulator,
because you are flying an actual
airplane in real-world motion with realworld
visuals," Mr. Weingarten explains.
In fact, pilots moving from TIFS to an
actual aircraft frequently remark that
the aircraft handles exactly the way that
TIFS simulated its handling. Further,
because TIFS allows pilots to operate
during simulated failures, it provides
them the opportunity to study and react
to dangerous situations in a safe vehicle
that can instantly revert to normal
control. Mr. Weingarten recognizes the
advantage this provides: "Often, you
don't want to fail a system on an [actual]
airplane, even in a test mode, because it
might be too dangerous to fly [as a
result]. Our airplane can do that safely."
TIFS' many benefits extend to
engineers as well. Normally, a test
aircraft will accumulate several hundred
hours of flight data, but "on the
ground, all engineers [can] do is look at
computer outputs, time histories,
graphs, and displays. But actually being
up there and experiencing all of the
little oscillations and responses brings a
sense of reality to the test. Flying helps
engineers to appreciate the problems that
they are investigating," Mr. Weingarten
asserts.
Highly versatile, TIFS uses two interchangeable
noses to perform a variety of
tests. Depending upon the type of
research, engineers can switch between
a simulation cockpit nose (see Figure 1)
and an avionics nose (see Figure 2)
called the Avionics System Test and
Training Aircraft (ASTTA) configuration.
In the simulation cockpit configuration, a test pilot flies TIFS,
which duplicates the characteristics of a
simulation model programmed into its
computer. During flight tests, the
computer adjusts TIFS' handling
characteristics by hydraulically
actuating
the plane's extra control surfaces,
including its side-force surfaces and
direct-lift flaps. The ASTTA configuration
lets TIFS perform avionics testing
using onboard radar, infrared electrooptical
detection systems, inertial
navigation, and a Global Positioning
System. For both configurations, TIFS
retains its safety cockpit, located above
and behind the nose. A pilot stands by
to take control and override the
simulation, if necessary.
TIFS has supported a variety of programs.
For instance, it aided National
Aeronautics and Space Administration
(NASA) researchers in developing a
cost-effective, next-generation supersonic
transport. Essentially, it helped
the NASA team evaluate the feasibility of
landing without forward visibility and
relying on sensors and displays alone. In
addition, AFRL scientists used TIFS to
evaluate an autonomous guidance and
control system for Boeing's X-40 Space
Maneuvering Vehicle.1 Recently, TIFS
supported an ITT Industries technology
known as ANGEL: Airborne Natural
Gas Emission LiDAR (Light Detection
and Ranging). ANGEL uses LiDAR
lasers to detect natural gas pipeline leaks
and identify their location within 10 ft of
the source, from a distance up to 1,000 ft
in the air. (See inset for a listing of
other TIFS-supported programs.)
TIFS' flexibility significantly expands
its capacity to support a wide variety of
programs.
In addition to changing nose
configurations, engineers can easily
modify TIFS to carry project-specific test
components such as sensors, computers,
or displays. Each project is different;
further, the evolving requirements
unique to this type of research have proven
the need for implementing continuous
updates. TIFS' simulation cockpit
configuration most recently gained a
new nose cap and canopy, adding room
to accommodate additional test equipment
comprising a new instrument
panel, side and center consoles, a rudder
pedal, throttle feel systems,
additional sensors, and displays including
a Silicon Graphics® computer and a
high-definition television camera.
Major Vincent Raska, TIFS project
manager, summarizes the resource: "It's
not as expensive as flying a jet airplane,
and its availability for testing is often
better than [that of] other aircraft such
as the C-17, C-5, or KC-135. Competing
for a test range can be a costly and timeconsuming
ordeal, but Calspan is
already approved by the Federal
Aviation Administration to fly in many
test areas." Maj Raska hopes TIFS will
be around for many years to come. "I
am all about recycling and reusing," he
states. "Despite being older, [TIFS] has
a lot of capability. It is very versatile and
flexible. It is one of a kind." Based in
Niagara Falls, New York, TIFS frequently
makes trips to different test locations
and is available to anyone in government
or industry requiring specialized
in-flight test capabilities.
Ms. Melissa Withrow (CACI), of the Air
Force Research Laboratory's Air Vehicles
Directorate, wrote this article. For more
information, contact TECH CONNECT at
(800) 203-6451 or place a request at
http://www.afrl.af.mil/techconn/index.htm.
Reference document VA-H-05-04.
Reference
1
Doman, D. and Withrow, M. "Integrated
Adaptive Guidance and Control." AFRL
Technology Horizons®, vol 5, no 6 (Dec 04):
47-48.