Physical Size Allocations for RF Electronics in Digital Beamforming Phased Arrays

2018-08-29

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Introduction

Phased array radars and active electronically scanned arrays (AESA) have been in use and deployed within the aerospace and defense market for well over a decade. This period began with primarily analog beamforming systems, with continual migration to higher levels of digital beamforming. System engineering objectives continually desire near elemental digital beamforming implementations for maximum flexibility and programmability.

There are many challenges associated with the migration to near elemental digital beamforming. The challenges range from calibration, digital control, distribution of clocks, LO, power, processing the volume of data, and the physical size constraints of the electronics. The prolific advancement of RF ICs for the wireless industry continues to enable the ability for higher levels of integration in RF designs and now practical implementations of every element digital beamforming arrays is becoming a reality.

In this article, we focus on the physical size requirements for the electronics. The physical size requirements as a function of the operating frequency are discussed, and practical implementation methods are reviewed.

Antenna Element Spacing vs. Frequency

First, consider the antenna element spacing as a function of frequency. To avoid grating lobes, an element spacing of λ/2 or less is required, where λ is the operating frequency wavelength.

Polarization diversity is also becoming a desired system objective. This feature provides the ability to program a variety of antenna polarizations including horizontal, vertical, or both left and right hand circular polarization. The antenna element implementation to achieve this feature is a radiating element with two ports, where each port radiates with orthogonal polarizations. By controlling the relative phase and amplitude of each port, the varied polarizations are created. Although a significant benefit for the system, this feature unfortunately doubles the number of antenna ports required and complicates the supporting electronics.

Equation 1

Figure 1 shows the element spacing vs. frequency, assuming there is a λ/2 antenna element spacing implementation. With these physical size constraints outlined, the RF subsystems behind the antenna can be evaluated to assess implementations required to meet the electronic channel spacing vs. frequency.

Figure 1. Element spacing vs. frequency.

Table 1. λ/2 Spacing for Select Frequencies
Frequency	Element Spacing	Dual Pole I/O Spacing
3 GHz	50 mm, 2 inches	25 mm, 1 inch
10 GHz	15 mm, 600 mils	7.5 mm, 300 mils
30 GHz	5 mm, 200 mils	2.5 mm, 100 mils

Waveform Generator and Receiver Channel Spacing

Figure 2 shows an evaluation board for one of the Analog Devices transceiver products. This board contains two transceivers. Each transceiver contains two transmit and receive channels (see Figure 3) and, thus, four complete waveform generators and receivers are implemented. The board also includes a clock IC and several other I/O features for evaluation of the parts.

Figure 3. Transceiver product line includes dual waveform generators and receivers.

Although the board was not intended for the highest level of integration possible, the board provides insight into practical size limits for the waveform generator and receiver section. It is quickly apparent from the board that the transceiver product line supports every element digital antenna spacing to C-band and, with some extra effort, an X-band element spacing could be realizable.

Next, the physical size of a mating RF up/downconverter is shown in Figure 4. This particular board is intended as a test board companion for the dual transceiver board and again can be used to consider practical physical size constraints for this RF subsystem. The board is implemented with standard low cost methods, using all commercially available parts. Again, this shows that this type of implementation supports every element digital antennas up to C-band. If there is a migration to X-band, every digital element would be possible, enabling further integration with SiP (system-in-package) integration.

Figure 4. X-/ku-band RF up/downconverter.

These two boards outline that low cost commercial implementations support every element in digital beamforming phased arrays for frequencies up to C-band. An every element implementation at X-band and beyond could be realizable with further integration or as alternative beamforming ICs can be used to reduce the number of waveform generator and receiver channels relative to the number of elements. 4:1 X-/Ku-band beamformers are now becoming commercially available and are a practical approach for low cost digital beamforming phased arrays at these frequencies.

Ka-Band Element Spacing

Next, a Ka-band antenna element spacing is considered, as shown in Figure 5. At 30 GHz the λ/2 spacing is 5 mm, which, as shown, is quite challenging for the electronics. It is practical, however, for a 4:1 analog beamformer to be implemented within this spacing directly opposite of the antenna elements. The challenge is that the physical size constraints allow little opportunity for additional components. This necessitates the need for the inclusion of LNAs or PAs within the beamforming package and for passive components, such as decoupling capacitors, to be buried within the PWB.

A fortunate design benefit for Ka-band satellite systems is that most systems separate transmit and receive functions into separate antennas. This provides the opportunity to design transmit only or receive only beamforming ICs optimized for the particular task.

Summary

The continued advancement of RF ICs for the wireless industry has become an enabler for the proliferation of digital beamforming phased array technology. It is now practical to design every element digital beamforming phased arrays with standard PWB technology for frequencies as high as C-band. At higher frequencies of X-band an every element digital implementation is practical, but extra design effort for further integration is likely required. Alternatively, a 4:1 analog beamformer could be used and offers additional space for the electronics and again allows for standard PWB implementation methods. This can become challenging at Ka-band physical size constraints. However, with integration of front-end electronics inside a beamformer package, either a subarrayed antenna architecture or an all analog beamforming system is now realizable.

关于作者

Peter Delos

Peter Delos是ADI公司航空航天和防务部的技术主管，在美国北卡罗莱纳州格林斯博罗工作。他于1990年获得美国弗吉尼亚理工大学电气工程学士学位，并于2004年获得美国新泽西理工学院电气工程硕士学位。Peter拥有超过25年的行业经验。其职业生涯的大部分时间都致力于高级RF/模拟系统的架构、PWB和IC设计。他目前专注于面向相控阵应用的高性能接收器、波形发生器和频率合成器设计的小型化工作。