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A121-001-R датащи(PDF) 17 Page - Acconeer AB

номер детали A121-001-R
подробное описание детали  Pulsed Coherent Radar (PCR)
PDF  24 Pages
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производитель  ACCOONEER [Acconeer AB]
домашняя страница  https://www.acconeer.com/
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A121-001-R датащи(HTML) 17 Page - Acconeer AB

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A121 Pulsed Coherent Radar (PCR)
Preliminary Datasheet v0.3
Page 17 of 24
2022-09-22
© 2022 Copyright by Acconeer
7.2 Sensor startup
The power-up and power-down sequences are shown in Figure 7.4.
Figure 7.4. Power-up and power-down sequences.
The power supplies VRX, VTX, VDIG and VIO can be turned on and off in any order. ENABLE
should be turned on after or simultaneously with VDIG and VIO, whichever is turned on last. The
A121 should however not be considered as in state “ON” until all supply voltage levels are stable and
ENABLE is high. The time constant t1 in Figure 7.4 denotes this time. The actual value of t1 depends
on the power supply and the decoupling capacitors used. Any I/O must be held at 0 V during time t1.
After power-up is complete, the sensor is ready for SPI communication and can be loaded with a
program. Up until the point where the sensor’s program is started, the INTERRUPT is in a high
impedance state. After the sensor’s program has started, the INTERRUPT is configured as a push-pull
CMOS output.
The power down sequence is initiated by setting ENABLE low. After that, all supplies can be turned
off. Any I/O inputs on A121 must be set to 0 V before or simultaneously with VIO going low to avoid
forward-biasing the internal ESD protection diodes.
7.3 Layout Recommendations
The sensor antennas are of a folded dipole type, with its main ground reference being the internal
package ground plane, extending below the whole area of the sensor. To further enhance the
directivity of the sensor, the package ground plane should be extended by soldering all GND pads to
the PCB top layer ground. In terms of regulatory compliance, any openings in the ground plane inside
the A121 footprint must be significantly smaller than the wavelength (5 mm in free space) to
effectively shield off any disturbance.
Figure 7.5 shows the simulated relative radar loop gain (RLG) as function of ground plane side length,
assuming a square ground plane. As the ground plane size increases, the RLG increases because of
increased antenna directivity. Constructive and destructive interference results in a non-monotonic
increase in RLG.
Time
VRX
VTX
VDIG
VIO
ENABLE
t1
t2



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