| PROTOTYPE
AND PROOF-OF-CONCEPT HARDWARE |
| Electrical |
 |
- Design classical textbook and
simulation methods.
- Motor controls (brushless three phase
DC, induction Brush) and power electronics.
- Signal processing (analog and
digital.)
- Data acquisition.
|
| Mechanical |
- Design - classical textbook and finite
element methods.
- Machining and sheet metal work.
- Packaging and enclosures.
|
| Control
Systems |
|
- Design - classical and modern methods.
- Simulation.
- Fabrication and testing of electrical,
hydraulic, and pneumatic systems.
|
| Mechanisms |
- Design and simulation.
- Side stick flight controllers, servo
valves, and actuators.
|
| ACTUATION
SYSTEM DESIGN ANALYSIS, TESTING |
| Control
System Design, Analysis & Testing |
- Electrical, hydraulic, and pneumatic
control systems.
- Analysis of linear and non-linear
systems using MATLAB, Simulink, and CC.
- Control system performance testing and
parameter measurement.
- Design and implementation of loading
systems.
- Fault tolerant design for critical
applications.
|
| Mechanical
Component Design & Fabrication |
|
- Structural, hydraulic, pneumatic, and
thermal design and analysis.
- Prototype and low rate manufacturing
(machining, material specification, sheet metal fabrication, and
assembly.)
|
| Electronic
Circuit Design & Fabrication |
|
- Power electronics.
- Motor controllers.
- Analog and digital circuit design.
- Printed circuit layout and assembly
(including surface mount technology.)
|
| CREATION
OF HIGH FIDELITY SIMULATION MODELS |
| Data
Acquisition & Analysis |
|
- Data acquisition systems design and
implementation (LabView and Visual Basic.)
- Data Analysis.
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| SYSTEM
INTEGRATION |
|
| System
Integration |
Software Development |
- System requirements development
and analysis.
- Hardware/software integration.
|
- C/C++, Visual Basic, and LabView.
- Real-time software design.
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| HIGHLIGHTS |
|
- Electrically Powered Actuator
Development (EPAD) Program – Flight test of three prototype
actuators in F/A-18 aileron location.
Smart Actuator - control and drive electronics moved from
flight control computer to actuator.
Communication over fiber optic link.
Electrohydrostatic actuator (EHA) and Electromechanical
actuator (EMA) - power-by-wire, control electronics mounted in
aircraft wing.
- X-37 – Actuation consultants,
specification compliance.
- X-38
– Crew re-entry vehicle prototype.
Design and implement flight control computer surrogate
system to verify performance of failure detection algorithm
software (FDIR). General
EMA, system, and integration consulting.
- X-43 – Actuation consultants.
Measure and verify on-vehicle performance of EMA’s.
Design and supply EMA stiffness measurement and dynamic
load testing system.
- Pilot Side-Stick Controller –
Assist with setup, test design, and data analysis of Dynamic
Controls designed and built flight control side-sticks in NASA
Dryden simulators.
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