Although the month of May 2000 was ordinary by most standards, it was
extraordinary for the Air Defense Artillery Test Directorate, U.S.
Army Operational Test Command. During the Patriot Advanced
Capabilities Configuration-3(PAC-3) Limited User Test (LUT) conducted at
Fort Bliss, Texas, simulation took its place as the main vehicle in an air
defense operational test. Over the course of approximately four weeks of
test time, crews of the test player unit, the 2nd Battalion, 1st Air
Defense Artillery, 35th ADA Brigade, Fort Bliss, engaged multiple
simulated Air-Breathing Threat (ABT) and Tactical Ballistic Missile (TBM)
targets in 120 realistic threat air battle scenarios. During this
phase of operational testing, not a single live aircraft or missile took
to flight. At the same time, however, all testing was effective in
terms of data adequacy and cost reduction. In fact, with
simulation at the helm via the PAC-3 Mobile Flight Mission Simulator (MFMS)
test tool, the cumulative cost of creating and engaging the enemy totaled
approximately $600 thousand--less than the cost of firing a single Patriot
missile.
The
MFMS Tool
At first glance, the MFMS appears to be an ordinary military vehicle (see
figure 1), but its capabilities extend far beyond that. The PAC-3
Configuration 3 MFMS is a hardware-in-the-loop (HWIL) test system for Patriot
that is able to simulate a variety of enemy air vehicles through
pre-programmed threat air battle scenarios. These threats include
various types of TBMs, ABTs, and Air-to-Surface Missiles (ASMs). The
threat targets have multiple arrival times and designated ground impact
points (GIPs) that require the Patriot system to engage multiple targets
simultaneously. The scenarios are not a random generation of
targets, but they are rather a true-to-life representation of known Patriot
threats across the globe. This feature significantly increases the
realism factor of the air battle in each scenario developed.
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Figure
1. Mobile Flight Mission Simulator. |
While
the mobility aspect of the simulator is relatively new, the origins of the
system are not. The Raytheon Corporation Patriot Program Office originally
conceived the Flight Mission Simulator (FMS) in 1974 with the purpose of
creating a tool for engineering and development. Eventually, Raytheon
intended to use the FMS tool for system developmental testing. The
idea was to exercise and test the Patriot system without altering its
tactical configuration. The fire unit equipment would be set up in
normal configuration and simply connected via the Patriot radar to the FMS
for artificial target insertion. Initial success came later that
year; this first version of the FMS was able to inject Radio Frequency (RF)
signals into the system radar for one simulated target. Within four
years, the FMS had the capability to stimulate the radar with up to 10
targets. Numerous software and hardware improvements have followed.
The test tool is now capable of stimulating the Patriot system with the
maximum number of targets allowed by the tactical system software.
Raytheon added mobility in 1995 by creating a truck-mounted FMS; this was
the evolution of the MFMS. Although engineering, development, and
developmental testing were the original intentions of the FMS, this
mobility allowed for tactical use and a bridge to the realm of operational
testing. After an extensive verification, validation, and
accreditation process according to Army Regulation 5-11 and Operational
Test Command Handbook 73-21, the MFMS was certified as a viable test tool.
The
test bed configuration is depicted photographically in figure 2 and
diagrammatically in figure 3. The Engagement Control Station (ECS)
is hardwired to the Radar Set (RS) and the RS is hardwired to the MFMS.
Additionally, the Communications Relay Group (CRG) van links by wire to
the ECS.
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Figure
2. The PAC-3 MFMS Testbed |
The
Information Coordination Central (ICC) communicates with the ECS via Patriot
Digital Information Link (PADIL), and it also communicates with the
Communications, Control, and Command Engineering Environment System
(C3EES) via Tactical Digital Information Link (TADIL) J. This is
done to emulate a Joint Defense Network and ensure the system is capable
of communicating in a joint environment via the TADIL-J messaging system.
The Battery Maintenance Center wires into the ECS to collect system
maintenance and status data via its Remote Maintenance Monitor (RMM) on
the Patriot Automated Logistics System (PALS) computer. Simulating
the Patriot Launching Stations are two Data Transfer Units (DTU).
One DTU in the ECS simulates local launchers, and the other DTU, located
in the CRG, simulates remote launchers which, in reality, may be in excess
of 10KM from the rest of the fire unit.
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Figure
3. MFMS Testbed Configuration. |
In
order to create the scripted targets for each scenario, the MFMS
stimulates the RS by inserting the RF signals necessary to emulate an
actual track of that type in the RS search sector.
When
the radar is operating in "active radiate" mode, a combination
of both MFMS-generated and real tracks will appear on the Patriot
manstations (operator scopes). Visually, the graphic representations of
MFMS tracks are no different than those of actual tracks. The
operator makes the differentiation between real and simulated tracks by
observing the Identify-Friend-or-Foe response of the track. Simply,
a real aircraft will generate an interrogation response whereas the
simulated aircraft will return no response.
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Figure
4. The Patriot Radar and MFMS Configured for Operation |
Why
Simulation?
With the testing of any new weapon system or upgrade to a fielded system,
there come two inevitable requirements. First, testing must
accurately mirror the system's operational environment, as it would exist
in its wartime mission. Second, and perhaps more challenging, is
that the first requirement must support the data collection required for
system evaluation and the corresponding test schedule. In the case of the
PAC-3 system, the absolute best test environment would be one of multiple
live TBM, ABT, and ASM targets in flight under tracking and engagement by
live PAC-3 missiles. This meets the first requirement as it mirrors Patriot
operations in a wartime environment. The stumbling block is that
costs would be monumental. With live missiles and aircraft flights
as costly as they are, simulation is the natural alternative.
Additionally, the continued proliferation of threat TBMs since Operation
Desert Storm makes the development of accurate threat representative
targets even more costly and challenging. The one simulation tool
that effectively satisfies much of the two operational testing
requirements for PAC-3 is the MFMS.
The
Bottom Line
The basic costs incurred differ immensely for one live Patriot missile
firing and the execution of one MFMS scenario. Based on PAC-3 Fiscal
Year 2001 live fire test projected costs, the funding required to fire a
single Patriot missile at White Sands Missile Range, New Mexico, is
approximately $2 million. This includes firing range time, cost of
the Patriot missile, and equipment maintenance primarily. Due to the
proximity of White Sands and Fort Bliss, equipment transportation is not
costly. Live missile firings at alternate locations, such as
Kwajalein Missile Range in the South Pacific, require as much as three
times the funding due to increased transportation and range operations
costs. The table below show additional expenditures that cause
overall costs to swell even further:
Additional
Expenditures |
Costs
due to research and developmental testing of the target missile
flight profile. |
Requirement
for multiple types of target missiles and target aircraft. |
Extensive
aircraft flying time requirements. |
Significant
wear-and-tear on the system as a result of live missile firings
would mandate extra repair parts and maintenance personnel. |
Increased
time requirements due to multiple missile reloads. |
Significant
coordination requirements and many points of failure. |
Based on PAC-3 LUT figures, the cost of one MFMS scenario with eight to 30
simulated target engagements is approximately $45 thousand. This
includes the operational costs of the equipment and the creation,
verification, and validation of the scenario for target adequacy.
The table below lists the multiple factors that result in significant
resource conservation.
Resource
Conservation Factors |
Much
simpler and more cost-effective verification and validation of
target flight profile for both missiles and aircraft; threat
missile motion modeling is much easier than reproducing a real
flying vehicle. |
Significantly
less system wear-and-tear and maintenance personnel requirements. |
No
physical reloads. |
No
flying time requirements . |
The
Outcome and Lessons Learned
The success of PAC-3 Limited
User Test reinforces the strength of simulation in operational testing.
The MFMS test tool allowed for required data collection and enabled the
conservation of multiple resources. With test costs always being a
factor throughout the projected fielding and evaluation of any system,
funding consistently weighs heavily on the mind of any Test Officer.
As in the case of PAC-3 and numerous other Department of Defense
systems-under-test, exact wartime conditions may not always be feasible in
terms of funding and manpower.
The
MFMS has demonstrated a proven capability to correctly simulate the flight
of threat aerial vehicles that, in turn, allows the operational tester to
collect system performance data. Additionally, the only critical
limitations of the MFMS are an incapability to simulate track clutter and
an incapability to stimulate more than one fire unit at a time.
Despite these few shortcomings, it is an outstanding tool that has lifted
strains on funding, personnel requirements, and man-hours for the Patriot
system. Its contributions will certainly allow for continued future
usage as a paradigm of a successful operational testing alternative.
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