ngVLA Enabling Technologies


Composite Antenna Development

In collaboration with the National Research Council (NRC) of Canada, the ngVLA is investigating the use of composite materials in the production of the ngVLA antennas, Figure 1. The proliferation of composite materials and production processes open up new conceptual options for large scale structures such as antennas, and may enable affordable, high-performance antenna designs.

NRAO’s expectation is that the technical requirements will not push technical boundaries but that the key challenge will be to deliver a design that can be manufactured in volume, delivered affordably, have low maintenance and total lifecycle costs.

The NRC ngVLA antenna design is based on the Single-piece Rim-supported Composite (SRC) reflector technology developed at NRC over the past decade.

The SRC concept has been successfully implemented in the DVA1 antenna, Figure 2, designed to work up to 10GHz, and in the DVA2 reflector, designed to work up to 50GHz. Both of these antennas used a tubular steel frame Back-Up Structure (BUS).

In scaling the concept to 18m it was found that it was not possible to meet the surface accuracy requirements for 116GHz operating frequency with the discrete attachment points between the BUS and reflector surface. A composite outer BUS (oBUS) was developed to provide a continuous support for the reflector surface, Figure 1,  enabling much higher surface accuracy under gravitational loading to be achieved.

The initial surface accuracy is largely dependent on the accuracy of the mold but in order to achieve and maintain the required surface accuracy NRC has developed a surface adjustment concept that incorporates a compliant connection between the oBUS and primary reflector surface and adjusters tangential to the surface around the perimeter.

The inner backup structure (iBUS) will be fabricated steel. The iBUS structure was designed using topology optimization software, and then the result rationalized to a manufacturable structure. The oBus panels are scalloped to provide discrete mounting points between iBUS and oBUS, addressing the mismatch in the coefficients of thermal expansion (CTEs) of the composite and steel parts of the structure.

Employing composite material technologies to the reflector can reduce ground spillover (no panel gaps), provide an even beam pattern that behaves predictably over temperature, and reduces the total mass of the reflector and backup structure. The later reduces the loads on the pedestal mount, improving pointing performance when compared to more traditional steel backup structures and aluminum reflectors.

 

ngDVA Concept Antenna

Figure 1: ngDVA Concept Antenna

NRC DVA-2 Prototype

Figure 2: NRC MK II Prototype (left), DVA-2 Prototype (center) and DVA-1 Prototype (right)

DVA-2 Surface

DVA-2 Surface Map with 335 um rms Surface Error


Integrated Receiver Development

The Integrated Receiver Development (IRD) program is an ongoing effort to develop modern integrated receiver architectures for radio astronomy that digitize early and are easier to manufacture and maintain in large numbers compared to conventional assemblies. A wide range of novel technologies has been developed, patented, and licensed in order to make these advancements possible.

At the core of this program is the idea that modern integrated electronics and digital signal processing (DSP) are complementary to each other. Numerical signal processing is capable of providing a level of flexibility and precision that is unachievable using purely analog means, while integrated technology provides the stable calibrations and smooth spectral baselines that are needed for the DSP to realize its full potential.

Each module is designed to immediately follow the cryogenic gain stage, and comprises everything that remains in the signal path operating at room temperature inside the antenna. This means that all conversions from RF-to-baseband, from analog-to-digital, and from copper-to-fiber are combined into a single, compact unit. Unique, multi-technology packaging and assembly techniques assure the best performance from micro-scale electronics with excellent digital-to-analog and channel-to-channel isolation.

The intrinsic receiver architecture is that of a single-stage, I/Q downconversion, using just one LO to get from the sky-frequency to baseband for immediate digitization. This allows for the earliest possible digitization in high-frequency systems while minimizing the potential for LO spurs and maximizing the instantaneous bandwidth for a given sample rate. Final separation of the I- and Q-channels into sidebands is deferred to the digital back-end for precise image-rejection, typically in excess of 50 dB, and is extremely stable over both time and temperature.

Integrated fiber-optic transceivers launch the raw, digital, I and Q data onto single-mode fibers with ranges of several meters to tens of kilometers. A unique, power-efficient, resolution-agnostic ADC-Serializer is under development which will further reduce power consumption. This will be supported in the back-end by a firmware IP block that can be installed on an FPGA platform and parses the data stream according to a novel, patent-protected algorithm. In this way, all the advantages of digital data transmission can be realized without most of the digital overhead normally required at the transmitter, such as bit-scrambling, packetizing, and framing.

While fabrication techniques vary by band, the overall concepts described above apply readily to the entire ngVLA frequency range. The most significant benefits of early digitization and the high level of stability afforded by these modules include reliability and scalability.

Integrated Receiver Schematic

Exploded view of W-band prototype.

IRD Block Diagram

Internal block diagram of a compact analog-digital-photonic receiver.

Integrated Receiver 2

S-Band prototype integrated receiver. 


Incoherent Clocking Development

In collaboration with the National Research Council of Canada, the ngVLA project is investigating novel techniques for phasing the array. Fundamentally in a coherent array it is necessary to continuously align the wavefront from the source prior to correlation and beamforming.  In the conventional approach, this is done using coherent LOs and digitizer clocks to do the high temporal-precision portion of this alignment, followed by digital delay and phase tracking according to a model of the wavefront delay for a known LO, and then periodic calibrator source observations to facilitate final alignment such that the “white light fringe”, on every correlated baseline, stays near zero relative delay.  However, the first part of this process can be done differently by using free-running and incoherent clocks at each antenna, measuring the phase/frequency of each one in a common clock domain, and then digitally correcting the data—amounting to delay and phase corrections—prior to wavefront delay+phase correction and correlation and beamforming. 

A block diagram of the general operation of the incoherent clocking method is shown in Figure 1.  Optional down conversion and digitization of data at each antenna occurs using its own independent LO frequency aLOn(t).  Digitized science data is sent to the correlator site along with a digital ‘tracer’ of aLOn(t) on a digital ‘tracer link’ (TL). The TL need only retain the real-time phase/frequency information of aLOn_tr(t) (the tracer frequency) inasmuch as needed to accurately extrapolate to the changing phase/frequency of aLOn_netLO(t) and aLOn_adc(t) that needs correcting in the data.  The frequency of the digital tracer is measured and tracked to very high accuracy using a digital tone extractor, as indicated in Figure 2.

Of course, changes in the tracer link delay, τ_TL(t), for any appreciable TL length has an effect on the measured tracer phase/frequency vs time as indicated in Figure 1.  To measure this, of course, a round-trip measurement is necessary: as shown in Figure 3, simply turn around the digital signal and measure its phase/frequency changes relative to the original digital tracer.  Use these measurements to adjust the aLOn_tr(t) measurement to obtain a ϕTL_n_est(t)-corrected estimate, aLOn_tr_est(t), of the antenna LO and use it for correcting the data. Once aLOn_est(t) is available, it is used to re-sample and, if necessary, phase-correct the data in the “Re-sampler/corrector” circuit, shown in more detail in Figure 4.  This circuit primarily consists of a real-time sample-by-sample interpolating O(80)-tap FIR filter, followed by a mixer to perform any phase corrections needed (for Nyquist zone-1 direct digitization, no phase corrections are required), driven by an aLOn_est- cLO phase synthesizer.  What comes out is digital data corrected into the common cLO clock domain, ready for correlation (and beamforming).

A demonstration system will be developed by NRC starting in the fall of 2018.

Incoherent Clocking Diagram 01

Figure 1: Block diagram of the general operation of the incoherent clocking method. Courtesty of NRC.

Incoherent Clocking Diagram 02

Figure 2: Block diagram to measure and track the aLOn_tr tracer digital tone using a digital complex tone extractor. Courtesty of NRC.

Incoherent Clocking Diagram 03

Figure 3: Digital round-trip measurement of the tracer, to remove tracer link delay variations, τ_TL(t), entangled in tracer phase/frequency measurements as an additional ϕTL_n(t) term. Courtesty of NRC.

Incoherent Clocking Diagram 04

Figure 4: The digital delay and phase correcting circuit. Courtesty of NRC.