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Engineer Control

Location:
Albuquerque, NM, 87113
Posted:
December 24, 2012

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Resume:

SALOMON J. QUINTANA

SUMMARY

I am a control system engineer interested in applied dynamics, simulation

and hardware implementation of control systems and digital algorithms for

electro-mechanical systems. I have 15 years' experience conceptualizing,

simulating and implementing control algorithms for electro-mechanical

systems, ranging from flight vehicle actuator control to gimbal based

optical imaging and directed energy weapons systems. I have experience

with hardware in the loop design. I have been the Principal Investigator

responsible for coordinating the team technical efforts and have served as

the lead control system engineer on various programs, implementing control

algorithms while working closely with the customer to ensure success of

these programs. My experience is primarily in control system development

and implementation for aerospace applications, but I have 2 years'

experience as a structural analyst as well. I have a bachelor's degree in

mechanical engineering and master's degree in electrical engineering. The

combination of having degrees in both mechanical and electrical engineering

and my experience base gives me the ability to understand control system

development from conceptualization to product delivery, and has led to the

deployment of successful operational systems of varying nature over the

course of my career. In many instances during my career, I have been asked

to control a process that I have not encountered before. I have researched

and self-studied the process and developed a successful control topology

numerous times over the years, and I am confident that I can have a

positive impact for any company in need of control system development for

dynamic systems, regardless of their nature.

A control system engineer will usually assume the system engineer role on a

project. Successful operation of a device under the influence of feedback

control requires the control engineer to be knowledgeable of the system

dynamics that govern the operation of the device, as well as the

environmental and operating conditions for the device. Successful hardware

deployment requires that the mechanical, electrical, and software designs

are implemented to support the control system design that will achieve the

performance goals, with the control engineer providing guidance to the team

to achieve the performance goals. I typically create top level

requirements from the underlying physics and environmental considerations

of the process and create requirements for the electrical, mechanical,

digital signal processing, and sensor subsystems that will support the

control system development. I assist the subsystem leads in constructing

cost and schedule estimates, perform risk analysis on aspects of the design

that are deemed higher risk functions, and perform simulation trade studies

to ensure a satisfactory design for the system being controlled. During the

integration and test phase, I create test plans and carry out then

functional and performance testing required to complete the control system

and product development to ensure the program will be completed on time and

on budget.

PROFESSIONAL SKILLS

. Top Secret Clearance while at Boeing SVS and Goodrich AeroSpace

Matlab, Simulink, xPC Target

MSC Nastran, NX Nastran, FEMAP

Demonstrated ability of deriving rigid body equations of motion, control

system and

Signal processing algorithms

. Demonstrated ability to self-study to acquire necessary skills to

complete work assignments

. I understand importance of system engineering tasks such as performing

trade studies, cost and scheduling, risk analysis, and requirements

definition.

EXPERIENCE

The following experience listing is not exhaustive; it highlights some

programs that detail the pertinent experience I have acquired in the area

of system analysis and control system implementation.

Senior Controls System Engineer

Feb 2011 to Sept 2012 Applied Technology Associates, Albuquerque, NM

. Next Generation Gimbal SBIR I was hired on to help the team produce a

working hardware demonstration of the Next Generation Gimbal, A concept

where rate of change of momentum wheels produce torque to actuate a

gimbaled telescope. I was able to apply my knowledge of rigid body and

motor dynamics to simulate and produce a working demonstration of how the

rate of change of angular momentum of two momentum wheels can be

controlled to actuate a gimbaled telescope, the benefit being the

creation of a low reaction torque device for space based applications.

o Specific Tasks

. Acting Principal Investigator

. Provide project manager with time and schedule updates

. Present material to customer in design reviews and technical

interchange meetings

. Create system simulation to support risk reduction, control

system, and digital algorithm validation

. Create test procedure

. Implement and debug control system and digital algorithms

architecture using the Matlab xPC Target.

. Documentation, including interim reports, final report, and

end user guide

. Tactical Inertial Unit SBIR I won an Air Force Small Business Innovative

Research Project (SBIR) Phase II award where I served as the Principal

Investigator for creating a miniaturized Optical Inertial Reference Unit

(OIRU). An OIRU is a gyro stabilized, flexure mounted mechanism from

which a collimated laser beam is mounted that serves as the precision

reference for a beam control application. I developed a detailed

schedule and requirements flow down to the electrical, mechanical, and

processing subsystems and led the technical team in development of the

unit. In addition to the principal investigator, I also was the lead

control system designer, performing simulation trade studies and risk

analysis on sensor selections and performance predictions for the unit

itself as well as top level simulations for the overall beam control

architecture the OIRU would reside in.

o Specific Tasks

. Principal Investigator responsible for technical approach

. Lead control system engineer responsible for feedback control

and digital algorithm design

. Interface with electrical, mechanical, and embedded software

engineers to create a detailed schedule

. Create requirements flow down to electrical, mechanical,

digital processing, and sensor subsystems

. Identify high risk elements of design and identify risk burn

down strategies

. Create system simulation to support risk reduction, control

system, digital algorithm validation, and design review

activities

. Present material to customer in design reviews and technical

interchange meetings

. Create test procedure

. Documentation, including interim reports and test procedures

Controls System Engineer

April 2005 to Feb 2011 CSA Engineering, Albuquerque, NM

. Relay Mirror Experiment SBIR I was the control system lead in creating

a conceptualization and implementation of control system modifications

to existing relay mirror experiment based at Starfire Optical Range,

Kirtland AF Base, ABQ NM. Laser weapons require direct Line of Sight

(LOS) from the source to the target to be effective. Some

applications do not have a direct LOS, and a relay mirror is needed to

transfer the incoming beam to the target, like in a situation where a

target is on the other side of a mountain; A relay mirror module can

be in an aircraft where the incoming beam is transmitted to the target

on the other side of the mountain, for example. There will be an

entire beam control system for the receive side optical system and an

entire beam control system for the transmit side optical system.

These two optical control systems were uncoupled in the relay mirror

experiment. I conceptualized and created a means of coupling the two

control systems by correcting the receive side residual error with the

transmit side high bandwidth jitter correction loop.

o Specific Tasks

. Lead control system engineer responsible for feedback

control and digital algorithm design

. Provided inputs to Principal Investigator for detailed

schedule

. Identify high risk elements of design and identify risk

burn down strategies

. Create system simulation to support risk reduction, control

system, digital algorithm validation, and design review

activities

. Create interface between customers control system and our

system

. Create test procedure

. Implement and debug control system and digital algorithms

architecture in the field

. Documentation, including interim reports and test

procedures

During testing, we only had 5 days to implement and test the

algorithm. We successfully integrated the algorithm and showed that by

coupling the control systems, the residual LOS error could be reduced

at the target, increasing the lethality of the weapon. The successful

implementation of the algorithm with such a short timeframe was

possible because I was diligent during the planning and simulation

stages of the effort. In the end, the project was successful, on

time, and under budget.

System Identification SBIR I created a time domain and frequency

domain system identification tool for structural systems based on the

Eigenvalue Realization Algorithm. The algorithm was tested on a

hexapod. The identified plant frequency response functions matched

the hardware consistently between 50-1000 Hz. The low frequency noise

lowered the signal to noise ratio of the accelerometers that were used

in the identification. Recently, I have applied wavelet de-noising

techniques to the system identification that reduces noise so that low

signal to noise signals can be better estimated at lower frequencies.

This has allowed the identification to provide better estimates to

lower frequencies.

Junior Structural Engineer I worked as a junior structural engineer on

various projects while at CSA. I gained experience with FEMAP and

Nastran. Though I am not a strong structural engineer, I am

functional at the craft of creating a mesh and running pertinent

analysis. More importantly, the experience did make me a stronger

control system engineer because I can interface with the structural

engineers easier having worked with their tools. For instance, given

this experience, it is much easier for me and the structural engineer

to share model information because I understand how he must set up his

models so that the coordinate systems he uses matches mine so that the

information I need from him can be incorporated into my models.

Controls System Engineer

May 2001 to April 2005 Goodrich Corporation, Albuquerque, NM

. Japanese Advanced Meteorological Instrument (JAMI). Supported system

integration and testing both in Albuquerque and at Customer's facility

for development of geosynchronous orbit satellite imaging system. I

was the control system engineer responsible for closing the control

loops and testing of the instrument at the Prime contractor's location

in Santa Barbara CA. During the final integration stages of the

effort, it was found that square wave commutation of the motors were

causing spikes in elevation axis Line of Sight of the instrument,

which would have made a billion dollar investment unusable in

geosynchronous orbit. With little margin for error and very little

time, we developed an algorithm that cancelled the LOS error spikes

caused by the commutation by creating a torque disturbance that we

would introduce. Using simulation as a guide, the algorithm measured

the amount of time samples it would take before a LOS of spike would

manifest as LOS error. Measuring the area underneath the spike, we

were able to create an algorithm that would cancel the commutation

spikes in an open loop sense. Open loop correction is very tricky.

The commutation events would occur at slightly different times with

temperature differences and our open loop correction would have to

change over temperature as well. Given the circumstances and the

gravity of the situation, our correction algorithm was a huge success

and ultimately allowed the instrument to be fielded.

o Specific Tasks

. Control system engineer responsible for implementing

feedback control system at the customers facility

. Create simulation to support spike correction cancellation

implementation risk reduction

. Create test procedure

. Implement and debug control system and digital algorithms

at customers facility

. Documentation

. Boeing Launch Vehicle Actuator Design. Lead control engineer for

development of control system for Boeing launch vehicle actuators.

Goodrich was asked by Boeing if they would be interested in being the

subcontractor in charge of the power electronic and control subsystem

for the project. A launch vehicle actuation system consists of gears

and ball screws arranged to give a mechanical advantage to control the

wing during flight. The power electronics (current and voltage

capacity of the drive) and gear/ball screw dynamics provide the force

capabilities of the actuator. I had no previous experience with this

type of mechanism, but my understanding of rigid body dynamics and

motor dynamics allowed me research and create a system model of the

process to enact control. The control topology chosen was to have an

input space angular rate loop (before gearing) and an output space

(after gearing) linear position loop with a dead band to account for

the backlash in the gears.

o Specific Tasks

. Lead control system engineer responsible for feedback

control and digital algorithm design

. Interface with subcontractors to create proper mechanical,

electrical, control system interfaces

. Identify suitable control system design that meets

requirements

. Identify high risk elements of design and identify risk

burn down strategies

. Create system simulation to support risk reduction, control

system, digital algorithm validation, and design review

activities

. Documentation, including interim reports and design reviews

Controls System Engineer

May 1997 to May 2001 SVS Inc., Albuquerque, NM

. Acoustic Cancellation SBIR Phase II Developed adaptive

feed-forward compensation technique to reduce acoustic

vibrations control in the ABL beam train. CSA Engineering

(whom I would eventually work for due to this project) was

working a Small Business Innovative Research (SBIR)

project to reduce the acoustic vibration of the Airborne

Laser beam train. They subcontracted SVS to help with

this because some of the senior engineers had some

understanding of adaptive filtering for directed energy

applications. The task was given to me, and I began self-

study on adaptive filtering, as I had no previous

knowledge of the field. In my studies, I found that there

was a more effective way of enacting feed forward adaptive

filter compensation under the influences of closed loop

control than what had been done before. If the reference

to the adaptive filter is filtered by the transfer

function from the point of injection into the loop to the

loop error signal, the adaptive filter will take into

account the fact that it is operating in a closed loop

system without having to account for this using block

diagram manipulation. Furthermore, the transfer function

can be determined via online system identification. These

two discoveries provided an improved adaptive filter

implementation for directed energy applications. This

version of an adaptive filter is very useful in closed

loop applications, and has found its way into numerous

directed energy applications.

o Specific Tasks

. Create adaptive feedforward cacellation technique for Air

Borne Laser program beam train vibration

. Create simulation to validate control system approach

. Documentation

EDUCATION

B.S., University of New Mexico, Albuquerque, NM, Mechanical Engineering,

May 1996.

M.S., University of New Mexico, Albuquerque, NM, Electrical Engineering,

May 2002.

Publications

Adaptive Feedforward Control for Adaptive Optic Systems, Directed Energy

Conference, ABQ NM, 2006

REFERENCES

Felix Morgan, PhD

Senior Control System Engineer

Currently Engineering Consultant

Formerly Goodrich Engineering Director That Hired Me

Formerly ATA Engineering Director That Hired Me

abgoxu@r.postjobfree.com

505-***-****

Victor Beazel, PhD

Dynamics and Controls Engineer

Government TPOC For Tactical OIRU Development

Kirtland Air Force Research Lab

505-***-****

Bill Chavez

Collegue, Life Long Friend

4617 Palo Duro Ave NE

Albuquerque NM 87110

505-***-**** (Cell)



Contact this candidate