Other Parts Discussed in Thread: MMWCAS-DSP-EVM, AWR1642BOOST, DCA1000EVM, AWR1642, IWR6843, IWR6843ISK, MMWAVEICBOOST
I would like to assemble a millimeter-wave radar transceiver system with the goal of collecting micro-Doppler signature signals generated by the rotation of rotors on multirotor UAVs. I have two proposed assembly schemes:
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Scheme 1: Connect the MMWCAS-RF-EVM to the MMWCAS-DSP-EVM, then to a PC. Two WR-12 25 dBi horn antennas are used to achieve signal gain. The horn antennas are connected to the MMWCAS-RF-EVM via a 1.0 mm-f to WR-12 waveguide transition, a 1.85 mm to 1.0 mm adapter, and a SMPM-m to 1.85 mm-f 5 cm cable. This configuration enables signal enhancement without modifying the original structure of the MMWCAS-RF-EVM.
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Scheme 2: Connect the AWR1642BOOST to the DCA1000EVM, then to a PC. Similarly, two WR-12 25 dBi horn antennas are used for gain, connected using a 1.0 mm-f to WR-12 waveguide transition, a 1.85 mm to 1.0 mm adapter, and a SMPM-m to 1.85 mm-f 5 cm cable, again without modifying the original structure of the AWR1642BOOST.
I would like to ask:
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Do either of these two assembly schemes have any technical issues or compatibility concerns?
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Which setup is more recommended?
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Will the signal resolution from either system, under open outdoor conditions, be sufficient to clearly display the micro-Doppler frequency shifts caused by different UAV models (i.e., variations in rotor length and rotational speed)?
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My UAV parameters are:
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Rotor length: 20–80 cm
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Propeller rotational speed: 2800–6000 RPM
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RCS: 0.02–0.2 m²
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If possible, I would also like to know the theoretical detection range of these systems under the given conditions, and whether the collected micro-Doppler features would be sufficient for UAV classification based on their signature differences.