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IMU
Sensors
In addition to the GPS output, the Tapestry system can generate high rate
Strapdown Inertial Measurement Unit (IMU) data comprised of
Dn
(incremental velocity) and Dq
(incremental attitude) using our proprietary multi-function I/O card (MFIO). The
card will generate the data in one of our predefined binary formats in
addition to a complete simulation of the hardware clock and handshaking
signals. The supported formats, LSB’s, and electrical interfaces include:
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Honeywell HG-1700
(SDLC) |  |
Rockwell Collins
GNP-10, GIC-100, IMU-202 |  |
Boeing DQS |  |
Litton LN-200 (SDLC) |
For the SDLC systems, the full CRC is generated along
with the navigation, autopilot, data interleaving, zero bit insertion, etc.
The user may define and configure the following model elements for the
system:
 | IMU
Case-to-BODY axis alignment |  | Accelerometer Bias, Scale Factor, White
and Correlated
noise. |  | Gyro
Bias, Scale Factor, White noise and Random walk. |
Our PCI multifunction I/O card (MFIO) resides within the computer
system expansion bus using high speed dual ported RAM. This interface, combined with a 5-element ring buffer, virtually
eliminates timing error between the generated RF and IMU data
outputs. The differential data interface is via a DB25 connector on the feature card.
The six-degree-of-freedom
vehicle motion generator included with the Tapestry system, constructs the Dn
and Dq
data automatically reflecting the simulated dynamics of the host vehicle. This
data is synchronized with the GPS RF signal and output to the feature card by
the run time executive. A 1-PPS reflecting the epoch timing of the synchronized
RF and IMU outputs is provided. The IMU electrical interface can be derived from
either and internal or external clock.
Navigation Laboratories Inc. (949)
766-0444, (949) 495-9551, Fax (949) 713-2479
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