RESUME
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Adults are always asking children what they want to be when
they grow up because they are looking for ideas.
-- Paula Poundstone
Michael Scott Heiman
DOB: 01/29/62
EDUCATION:
BSME Purdue University Spring 1984
MSME Purdue University Summer 1986 - Master's Thesis option:
academic work stressed control systems and applied dynamics.
September 1999 - Present
Control Systems Research
- (Headhunters shalt not call me at work. Final
Warning!)
Crestview, FL
Control Systems Research is currently developing a
systems integration toolkit that can be used for developing real-time, HWIL
simulations that use INSs and GPS receivers. The toolkit is written in
C++ and runs on the Microsoft Windows 2000 operating system. My
responsibilities include the development of the simulation modules (generic
aircraft, INS, GPS receiver, and GPS satellite constellation), Ethernet
interfaces (to the L3 SCS-2450 Satellite Constellation
Simulator (SCS), the Local Object Broker at the AFRL IDAL Laboratory, and the
simulation modules), and the Test Asset Modules (which are C++ wrappers that
encapsulate the MIL-STD-1553 bus messages defined in the SNU-84 ICD,
ICD-GPS-059, JDAM Core ICD, F22-GINS ICD, and (eventually) the Honeywell EGI
ICD).
Currently developing an integration test bed for
the AFRL IDAL at Wright-Patterson AFB, OH. This test bed integrates
and time synchronizes internal and external 6DOF aircraft simulations with
various HW. The test bed uses the simulated motion data to stimulate
the SCS, other RF stimulators, and (eventually) the Honeywell EGI (an
integrated INS/GPS navigator). When finished, this test bed will allow
the IDAL to integrate prototype aircraft subsystems with existing navigation
systems and test the hardware in a simulated dynamic environment.
Developed a prototype systems integration test bed
that allows aircraft subsystems to communicate via a MIL-STD-1553 bus.
The test bed allowed an operator to initialize and control an INS, a GPS
receiver, and a JDAM. The test bed uses data extracted from the INS
and the GPS receiver to initialize the JDAM and simulate a release.
The final version of the test bed software (MTVCOM) has been installed in
the Mobile Test Van at the AFRL, Eglin AFB, FL. MTVCOM allows Air
Force personnel to test the JDAM's capability to acquire and track GPS
satellites in a real world environment. CSR and the Air Force plan to
extend MTVCOM's capabilities to test other systems in stationary or low
dynamic environments.
Developed a real-time trajectory generator that controlled
a real-time GPS signal simulator (an L3 SCS-2400 Satellite Constellation
Simulator and a Global Simulations System (GSS) Satellite Simulator). Implemented real-time INS algorithms that propagated a
navigation solution using discrete INS measurements. Developed real-time
visualization tool using Multigen-Paradigm's Vega software (and really don't
care to use Vega again.) Gained programming experience in Windows
sockets, TCP/IP, multi-tasking, multi-threaded applications.
August 1988 - September 1999
Sverdrup Technology Inc./TEAS Group
Eglin AFB, FL
Sverdrup Technology is the prime contractor for the
Technical Engineering and Acquisition Support (TEAS) Contract.
Sverdrup's role is to support the Air Force in the development, test, and
acquisition of conventional weapon systems at Eglin AFB, Florida.
My specialty was the evaluation of autonomous weapon
systems. I have been involved in various programs that have integrated
seekers with inertialy aided munitions. I have experience in
evaluating weapon systems that use the Global Positioning System (GPS),
inertial navigation systems (INS), various guidance and control laws,
extended Kalman filters, mission planning systems (for autonomous weapons),
autonomous acquisition and tracking algorithms, and various seeker
technologies. I have developed a variety of simulations - ranging from
simple covariance analysis simulations to high fidelity 6-DOF simulations -
that have been used to evaluate these systems. I have developed
simulations and analysis tools on a variety of platforms (VAX, UNIX, DOS,
and MS Windows) and in several languages (FORTRAN, C, C++, MatLab, MatrixX,
and (unfortunately) Ada). I have designed autopilots, guidance laws,
and Kalman filters to support concept exploration studies for the Air Force.
November 1997 - September 1999: Supported the Air
Force Research Laboratory (AFRL) Simulation and Assessment Branch.
Also supported the Demonstration of Advanced Solid State LADAR (DASSL)
Program. This program will design an autonomous LADAR seeker that will
be attached to an INS/GPS guided munition. My role was to design and
develop a variety of simulations to assess the performance of the guided
munition.
1994 - September 1999: Supported the AFRL on the
Advanced Synthetic Aperture Radar Guidance (ASARG) and Hammerhead Programs.
The Hammerhead Program was attaching an autonomous synthetic aperture radar
that was developed on ASARG to an INS/GPS guided munition. My roles
were to develop and design a 6-DOF simulation of the munition, evaluate
system performance, and interact with the Test Wing to ensure that test
objectives could be met.
1996 - October 1997: Supported the AFRL on the Low
Cost Autonomous Attack System (LOCAAS) Program. This program will
develop a submunition that will autonomously identify and attack mobile
targets. My task was to use a contractor delivered simulation to
evaluate the performance of the system against moving targets, design
alternative Kalman filters to enhance performance, and mentor a journeyman
engineer while he developed data visualization software.
1993: Supported the Air Force by developing a
covariance analysis simulation of a INS/GPS munition that used an imaging
infrared seeker. This simulation was later modified to support the
ASARG program.
1988-1992: Supported the Air Force on the Autonomous
Guidance for Conventional Weapons (AGCW) Program. This program
developed an autonomous imaging infrared seeker that was attached to an
inertialy guided munition. My role was to work with a group to develop
a high fidelity simulation of the weapon system.
1986-1988
Hughes Aircraft Company
Missile Systems Group
Tucson, AZ
Assigned to the TOW Missile Laboratory. Tasks
included the development, maintenance, and use of simulations to support TOW
missile development. Designed the roll autopilot for the TOW 2A
system.