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DESCRIPTION
The LRA-2100 is Rockwell Collins first digital radio altimeter allowing
increased precision while transmitting less power and consuming a fraction
of the power of traditional radio altimeters. This is made possible through
the use of the latest digital technology - specifically dual independent digital
signal processors (DSP). Using DSP technology, the LRA-2100s altitude algorithm can compute
the fast fourier transform (FFT) spectral analysis of the signal returned
from the terrain below. The spectral analysis algorithm used within the LRA-2100
provides the ability to discriminate terrain within the spectrum. This new
capability allows for enhanced altitude reporting such as multi-target adaptation
for fewer auto-pilot disconnects, bright spot rejection, and rejection of
under-flying aircraft. Another feature of this technology is significantly
improved performance over runway approach structures. Utilizing independent
dual DSP technology it allows for tight cross comparison of the data to ensure
integrity and safety. The LRA-2100 benefits from moving from analog to digital technology
by using minimal analog circuitry and a lower overall component count, which
increases the overall reliability of the system. The 40% lower power consumption
allows the LRA-2100 to not require forced air cooling and reduces the total
weight by an incredible 25% of similar radio altimeters. The LRA-2100 outputs a maximum of 26.5dBm (0.5W). A direct digital
synthesizer (DDS) used within the RF transmitter to control the FM/CW is attributed
to the increased altitude accuracy and lower RF power output. The LRA-2100 is used to provide extremely high altitude accuracy above
terrain to the pilot during approach and landing phases of flight. Accurate
altitude information during approach and landing phases is crucial to autopilot
and auto-landing systems, such as the Automatic Flight Control System (AFCS),
that require high integrity accurate altitude information. The data is also
a critical input to the Terrain Awareness and Warning System.
TYPICAL SYSTEM | LRA-2100 | 822-0334-020 | Radio Altimeter Transceiver.
-20 to 5500 ft altitude range. Full performance monitoring for all single,
dual, and triplex installations. Category III autoland capability. Meets
all critical level HIRF requirements. Conforms to DO-178B/DO-160E /DO254
requirements. Enhanced BITE interface. Retrofits LRA-900. | Airbus A320/A330/ A340/A380/ A350 |
SPECIFICATIONS FAA TSO | -C87 | Environmental | A2C4D1/XBC/CLY/XXXXXXZEAEZYZKXX | RTCA Documents | DO-155, DO-160E, DO-178B,
DO-254 | EUROCAE | ED-30,
ED-12A, ED-14C | ARINC Char. | 600,429,707 |
Height | 195.6
mm (7.7 in) | Width | 92.4 mm (3.64 in) | Length | 396.2
mm (15.6 in) | Weight | 3.81 kg (8.39 lb) | Size | 3 MCU |
Temperature | DO-160E Cat A2/C4/D1 Operational
Temperature-40° to +70°C Ground Survival Temperature -55° to +85°C | Altitude | Max
altitude 15200 m (50000 ft) |
Input Power | 115 Vac, 400 Hz, nominal 97
Vac, 360 Hz, minimum 134 Vac, 800 Hz, maximum 115
Vac, 400 Hz, nominal 26 Vac, nominal |
Center Frequency | 4300 ± 10 MHz | Frequency
Deviation | ± 150 MHz | Transmitter Power | 400 mW | Altitude
Range | -6.1 to 1748 m (-20 to 5700 ft) | Accuracy | BNR: 0.04 m (0.125 ft),
BCD: 0.03 m (0.10 ft) | Resolution | 400
mW | Tracking Capability | 400 mW | Data
Output | 400 mW | Antenna Requirements | 400 mW | Aircraft
Installation Delay (AID) | 400 mW |
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