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Goddard
Space Flight Center
2000 Phase 2
Magneto hydrodynamic (MHD) Stable Reference (MSTAR)
Applied Technology Associates
Albuquerque, NM
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INNOVATION
Several important innovations were introduced and demonstrated in
the MHD Inertial Reference Unit (MIRU) prototype. The prototype design
created for the MIRU addressed all of the critical components needed
to achieve the requisite performance of a high-quality optical IRU.
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Generalized Optical Control Line-of-Sight System
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ACCOMPLISHMENTS
- Design a configuration that facilitates separation of the sensors
for low-frequency LOS knowledge and the sensors for high-frequency
LOS stabilization.
- The prototype MIRU was modeled in detail to facilitate prediction
of performance and to allow comparisons of verification test results
with predictions. Excellent agreement was achieved between predictions
and measurements.
- Currently available digital processing technology enabled the implementation
of the prototype MIRU hybrid configuration and succeeded in achieving
performance better than 100-nradians.
system
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COMMERCIALIZATION
- The NASA-sponsored SBIR project
has opened the door for ATA to bid on an optical IRU production program.
- The United States Air Force and the MDA have also actively solicited
R&D efforts for ATA’s optical inertial reference units and
related technology innovations to achieve 20 nano-radian stability.
- ATA and aerospace companies have
initiated discussions that involve solicitation of technical, design,
and manufacturing support from ATA to deliver additional optical inertial
reference units for terrestrial, airborne and space applications in
long line-of-sight optical systems.
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GOVERNMENT/SCIENCE
APPLICATIONS
- A variety of NASA, Air Force, other military, and commercial opportunities
exist for the MIRU system and also its component technologies. The
marketing opportunity space is driven by requirements associated with
advanced optical systems, with performance objectives that require
precise LOS pointing and stabilization.
- As ATA performed the integration and test of the prototype MIRU,
the company became aware of a potential application that meshed with
future NASA needs. MIRU III, the third generation MIRU is being built
for MIT/LL for use in the Mars Laser Communications Demonstration
Program to point the laser from the Mars orbiter to Earth receiving
stations.
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Manufacturing/Fabrication
, Optics
, Sensors
Curator: SBIR
Support 8/23/05
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