Monthly Archives: February 2014

EMERGING TECHNOLOGIES

Several new technologies are being developed that are not specifically defined in the NAS. One technology that will in­crease system capacity is the roll-out and turn-off (ROTO) system. The ROTO system reduces runway occupancy time for arrivals by providing guidance cues to high-speed exits. The ROTO system with a heads-up display gives steering and braking cues to the pilot. The pilot is able to adjust braking and engine reversers to maintain a high roll-out speed while reaching the exit speed at the appropriate time. In low visibil­ity, ROTO outlines the exit and displays a turn indicator. Present ROTO development uses steering cues to exit the runway; future systems could provide automatic steering ca­pability (11).

APPLICATIONS AND IMPACT ON SYSTEMS

Antennas enjoy a very large range of applications, both in the military and commercial world. The most well-known applica­tions of antennas to the average person are those associated with radio, TV, and communication systems. Today, antennas find extensive use in biomedicine, radar, remote sensing, as­tronomy, navigation, radio frequency identification, control­ling space vehicles, collision avoidance, air traffic control, GPS, pagers, wireless telephone, wireless local area networks (LANs) etc. These applications cover a very wide range of fre­quencies as shown in Table 1 (2,3,40):

Antennas in Communication Systems

Antennas are one of the most critical components in a commu­nication system since they are responsible for the proper transmission and reception of electromagnetic waves. The an­tenna is the first part of the system that will receive or trans­mit a signal. A good design can relax some of the complex system requirements involved in a communication link and increase the overall system performance.

The choice of an antenna for a specific application (cellular, satellite based, ground based, etc.), depends on the platform to be used (car, ship, building, spacecraft, etc.), the environ­ment (sea, space, land), the frequency of operation, and the nature of the application (video, audio data, etc.). Communi­cation systems can be broken into several different categories:

Direct (Line-of-Site) Links. A transmission link established between two highly directional antennas. The link can be be­tween two land-based antennas (radio relays); between a tower and a mobile antenna (cellular communication); be­tween a land-based antenna and a satellite antenna (earth- space communication); between two satellite antennas (space communication). Usually these links operate at frequencies between 1 to 25 GHz. A typical distance between two points in a high capacity, digital microwave radio relay system is about 30 miles.

Satellites and Wireless Communications. Antennas on or­biting satellites are used to provide communications between various locations around the earth. In general, most telecom­munication satellites are placed in a geostationary orbit

Table 1. Frequency Bands and General Usage

Band

Frequency

Designation

Range

Usage

Very low fre­

3-30 kHz

Long distance telegraphy, nav-

quencies

igation. Antennas are physi-

(VLF)

cally large but electrically small. Propagation is accom­plished using earth’s surface and the ionosphere. Verti­cally polarized wave

Low frequency

30-300 kHz

Aeronautical navigation ser-

(LF)

vices, long distance commu­nications, radio broadcast­ing. Vertical polarization

Medium fre-

300-3000 kHz

Regional broadcasting and

quency (MF)

communication links, AM radio

High frequency

3-30 MHz

Communications, broadcast-

(HF)

ing, surveillance, CB radio (26.965-27.225 MHz). Iono­spheric propagation. Vertical and horizontal propagation

Very high fre­

30-300 MHz

Surveillance, TV broadcasting

quency (VHF)

(54-72 MHz), (76-88 MHz), and (174-216 MHz), FM ra­dio (88-108 MHz). Wind pro­filers

Ultra high fre-

300-1000 MHz

Cellular communications, sur-

quency (UHF)

veillance TV (470-890 MHz)

L

1-2 GHz

Long range surveillance, re­mote sensing

S

2-4 GHz

Weather, traffic control, tracking, hyperthermia

C

4-8 GHz

Weather detection, long range tracking

X

8-12 GHz

Satellite communications, mis­sile guidance, mapping

Ku

12-18 GHz

Satellite communications, al­timetry, high resolution mapping

K

18-27 GHz

Very high resolution mapping

Ka

27-40 GHz

Airport surveillance

Submillimeter

Experimental stage

waves

satellites operate at the L, S, or Ku band, but increasing de­mand for mobile telephony and high speed interactive data exchange is pushing the antenna and satellite technology into higher operational frequencies (47). Future satellites will be equipped with antennas at both the Ku and the Ka bands. This will lead to greater bandwidth availability. For example, the ETS-VI (A Japanese satellite comparable to NASA’s TDRS), carries five antennas: an S-band phased array, a 0.4 m reflector for 43/38 GHz, for up and down links, an 0.8 m reflector for 26/33 GHz, a 3.5 m reflector for 20 GHz, and a 2.5 m reflector for 30 GHz and 6/4 GHz. Figure 10 shows a few typical antennas used on satellites. It is expected that millions of households, worldwide, will have access to dual Ku/Ka band dishes in the twenty-first century. These house­holds will be able to enjoy hundreds of TV channels from around the world. Moreover, low cost access to high speed, voice, data, and video communications will be available to more customers (48).

Personal/Mobile Communication Systems. The vehicular an­tennas used with mobile satellite communications constitute the weak link of the system. If the antenna has high gain, then tracking of the satellite becomes necessary. If the vehicle antenna has low gain, the capacity of the communication sys­tem link is diminished. Moreover, hand-held telephone units require ingenious design due to lack of ‘‘real estate’’ on the portable device.

There is more emphasis now in enhancing antenna tech­nologies for wireless communications, especially in cellular communications, which will enhance the link performance and reduce the undesirable visual impact of antenna towers. Techniques that utilize ‘‘smart’’ antennas, fixed multiple beams, and neural networks are now being utilized to in­crease the capacity of mobile communication systems, whether it is land-based or satellite-based (49). It is antici­pated that in the twenty-first century the ‘‘wire’’ will no longer dictate where we must go to use the telephone, fax, e­mail, or run a computer. This will lead to the design of more compact and more sophisticated antennas.

Satellite

JK

Satellite dish

Satellite dish

APPLICATIONS AND IMPACT ON SYSTEMS

(GEO), about 22,235 miles above the earth as shown in Fig.

1. There are also some satellites at lower earth orbits (LEOs) that are used for wireless communications. Modern satellites have several receiving and transmitting antennas which can offer services such as video, audio, data transmission, and telephone in areas that are not hard-wired. Moreover, direct – TV is now possible through the use of a small 18-inch reflector antenna with 30 million users in the U. S. today (41,42).

Satellite antennas for telecommunications are used either to form a large area-of-coverage beam for broadcasting or spot beams (small area-of-coverage) for point-to-point communica­tions. Also, multibeam antennas are used to link mobile and fixed users that cannot be linked economically via radio, land – based relays (43-46).

The impact of antennas on satellite technology continues to grow. For example, very small aperture terminal dishes (VSAT) at Ku band that can transmit any combination of voice, data, and video using satellite networking, have become valuable tools for several small and large companies. Most

APPLICATIONS AND IMPACT ON SYSTEMS

47.1 ft

Ka-band command, ranging, and telemetry antennas

7.2-ft, 30-GHz receiving antenna

29.9 ft

10.8-ft,

20-GHz

transmitting

antenna

3.3-ft steerable antenna

Solar array7

^5>

Figure 10. Typical antennas on a satel­lite. (Courtesy, NASA Lewis Center)

Dual subreflectors

Antennas for Biomedical Applications

In many biological applications the antenna operates under very different conditions than the more traditional free-space, far-field counterparts. Near fields and mutual interaction with the body dominate. Also, the antenna radiates in a lossy environment rather than free space. Several antennas, from microstrip antenna to phased arrays, operating at various fre­quencies, have been developed to couple electromagnetic en­ergy in or out of the body. Most medical applications can be classified into two groups (50): (1) therapeutic and (2) infor­mational. Examples of therapeutic applications are hyper­thermia for cancer therapy, enhancement of bone and wound healing, nerve simulation, neural prosthesis, microwave angi­oplasty, treatment of prostatic hyperlastia, and cardiac abla­tion. Examples of informational applications are tumor detec­tion using microwave radiometry, imaging using microwave tomography, measurement of lung water content, and do­simetry.

Therapeutic applications are further classified as invasive and noninvasive. Both applications require different types of antennas and different restrictions on their design. In the noninvasive applications (not penetrating the body), antennas are used to generate an electromagnetic field to heat some tissue. Antennas such as helical-coils, ring capacitors, dielec­trically loaded waveguides, and microstrip radiators are at­tractive because of their compactness. Phased arrays are also used to provide focusing and increase the depth of penetra­tion. The designer has to choose the right frequency, size of the antenna, and the spot size that the beam has to cover in the body. The depth of penetration, since the medium of propagation is lossy, is determined by the total power applied or available to the antenna. Invasive applications require some kind of implantation in the tissue. Many single anten­nas and phased or nonphased arrays have been extensively used for treating certain tumors. A coaxial cable with an extended center conductor is a typical implanted antenna. This type of antenna has also been used in arteries to soften arterial plaque and enlarge the lumen of narrowed arteries.

Antennas have also been used to stimulate certain nerves in the human body. As the technology advances in the areas of materials and in the design of more compact antennas, more antenna applications will be found in the areas of biol­ogy and medicine.

Radio Astronomy Applications

Another field where antennas have made a significant impact is the field of astronomy. A radio telescope is an antenna sys­tem that astronomers use to detect radio frequency (RF) radi­ation emitted from extraterrestrial sources. Since radio wave­lengths are much longer than those in the visible region, radio telescopes make use of very large antennas to obtain the resolution of optical telescopes. Today, the most powerful radio telescope is located in the Plains of San Augustin, near Sorocco, N. M. It is made of an array of 27 parabolic antennas, each about 25 m in diameter. Its collecting area is equivalent to a 130-m antenna. This antenna is used by over 500 astron­omers to study the solar system, the Milky Way Galaxy, and extraterrestrial systems. Puerto Rico is the site of the world’s largest single-antenna radio telescope. It uses a 300-m spheri­cal reflector consisting of perforated aluminum panels. These panels are used to focus the received radio waves on movable antennas placed about 168 meters above the reflector surface. The movable antennas allow the astronomer to track a celes­tial object in various directions in the sky.

Antennas have also been used in constructing a different type of a radio telescope, called radio interferometer. It con­sists of two or more separate antennas that are capable of receiving radio waves simultaneously but are connected to one receiver. The radio waves reach the spaced antennas at different times. The idea is to use information from the two antennas (interference) to measure the distance or angular position of an object with a very high degree of accuracy.

Radar Applications

Modern airplanes, both civilian and military, have several an­tennas on board used for altimetry, speed measurement, colli­sion avoidance, communications, weather detection, naviga-

APPLICATIONS AND IMPACT ON SYSTEMS

Figure 11. A basic radar system.

tion, and a variety of other functions (40,51-53). Each function requires a certain type of antenna. It is the antenna that makes the operation of a radar system feasible. Figure 11 shows a block diagram of a basic radar system.

Scientists in 1930 observed that electromagnetic waves emitted by a radio source were reflected back by aircrafts (echoes). These echoes could be detected by electronic equip­ment. In 1937, the first radar system, used in Britain for di­rection finding of enemy guns, operated around 20 MHz to 30 MHz. Since then, several technological developments have emerged in the area of radar antennas. The desire to operate at various frequencies led to the development of several, very versatile and sophisticated antennas. Radar antennas can be ground-based, mobile, satellite-based, or placed on any air­craft or spacecraft. The space shuttle orbiter, for example, has 23 antennas. Among these, four C-band antennas are used for altimetry, two to receive and two to transmit. There are also six L-band antennas and 3 C-band antennas used for naviga­tion purposes.

Today, radar antennas are used for coastal surveillance, air traffic control, weather prediction, surface detection (ground penetrating radar), mine detection, tracking, air-de – fense, speed-detection (traffic radar), burglar alarms, missile guidance, mapping of the surface of the earth, reconnais­sance, and other uses.

In general, radar antennas are designed as part of a very complex system that includes high power klystrons, traveling wave tubes, solid state devices, integrated circuits, comput­ers, signal processing, and a myriad of mechanical parts. The requirements on the radar antennas vary depending on the application (continuous wave, pulses radar, Doppler, etc.) and the platform of operation. For example, the 23 antennas on the space shuttle orbiter must have a useful life of 100,000 operational hours over a ten-year period or about 100 orbital missions. These antennas are required to operate at tempera­tures from -150 °F to 350 °F during re-entry. The antennas also have to withstand a lot of pressure and a direct lightning strike. The antenna designer will have to meet all of these constraints along with the standard antenna problems of po­larization, scan rates, frequency agility, etc.

Impact of Antennas in Remote Sensing

Remote sensing is a radar application where antennas such as horns, reflectors, phased arrays, and synthetic apertures are used from an airplane or a satellite to infer the physical properties of planetary atmosphere and surface or take im­ages of objects.

There are two types of remote sensing: active and passive (radiometry) and both are in wide use. In the active case a signal is transmitted and the reflected energy, intercepted by the radar as shown in Figure 12, is used to determine several characteristics of the illuminated object such as temperature, wind, shape, etc. In the passive case the antenna detects the amount of microwave energy radiated by thermal radiation from the objects on the earth. Radiometers are used to mea­sure the thermal radiation of the ground surface and/or atmo­spheric condition (13,54-56).

Most antennas associated with remote sensing are down­ward-looking, whose radiation patterns possess small, close – in sidelobes. Remote sensing antennas require a very careful design to achieve high beam efficiency, low antenna losses, low sidelobes, and good polarization properties. Ohmic losses in the antenna is perhaps the most critical parameter since it can modify the apparent temperature observed by the radiom­eter system.

The degree of resolution of a remote map depends on the ability of the antenna system to separate closely space objects in range and azimuth. To increase the azimuth resolution a technique called ‘‘synthetic aperture’’ is employed. Basically, as an aircraft flies over a target the antenna transmits pulses assuming the value of a single radiating element in a long array. Each time a pulse is transmitted, the antenna, due to the aircraft’s motion, is further along the flight path. By stor­ing and adding up the returned signals from many pulses, the single antenna element acts as the equivalent of a very large antenna, hundreds of feet long. Using this approach, an an­tenna system can produce maps approaching the quality of good aerial photographs. This synthetic aperture antenna be­comes a ‘‘radio camera’’ that can yield excellent remote imag­ery. Figure 13 depicts a reflectivity map of the earth taken by NASA’s scatterometer.

Today, antennas are used in remote sensing applications for both the military and civilian sectors. For example, in the 1960s the US used remote sensing imaging from satellite and airplanes to track missile activities over Cuba. In the 1970s, remote sensing provided NASA with needed maps of the lu­nar surface before the Apollo landing. Also in July 1972, NASA launched the first earth resource technology satellite (ERTS-1). This satellite provided data about crops, minerals, soils, urban growth, and other earth features. This program

APPLICATIONS AND IMPACT ON SYSTEMS

APPLICATIONS AND IMPACT ON SYSTEMS

Figure 13. A reflectivity map of the earth taken by NASA’s Scatterometer. (Courtesy, NASA/ JPL)

still continues its original success using the new series of sat­ellites called the Landsats. In 1985, British scientists noted the ozone depletion over Antarctica. In 1986, US and French satellites sensed the Chernobyl nuclear reactor explosion that occurred in Ukraine. Landsat images from 1975 to 1986 proved to be very instrumental in determining the deforesta­tion of the earth, especially in Brazil. In 1992, hurricane An­drew, the most costly natural disaster in the history of the United States, with winds of 160 miles per hour, was detected on time by very high resolution radar on satellites. Because of the ability to detect the hurricane from a distance, on time, through sophisticated antennas and imagery, the casualties from this hurricane were low. In 1993, during the flooding of the Mississippi River, antenna images were used to assist in emergency planning, and locating threatened areas (56). In 1997, NASA, using antennas, managed to receive signals from Mars and have the entire world observe the pathfinder maneuver itself through the rocky Martian terrain.

Final Processing

Twisting. Just before a multifilamentary strand has reached final size, it is usually twisted about its drawing axis. The twisting is required to reduce flux-jump instabil­ity caused by varying external fields, reduce instabilities caused by self-field, and reduce eddy-current losses. The tightness of the required twist increases with the expected rate of change of field. The required twist pitch for a super­conducting supercollider strand, a relatively steady-state magnet, was approximately 80 rotations along the draw­ing axis per meter, while for ac application with a similarly sized strand the number of twists per meter might be 300. The twisting occurs just before the strand is reduced to fi­nal size so that it can be locked in by a final drawing pass or by final shaping.

Final Shaping. The final shape of the strand cross section need not be round in cross section: It can also be shaped into square or rectangular cross section by the use of in­dependently adjusted rollers operating along the strand surface.

Cabling. Individual strands can be cabled or braided to­gether to form a conductor with a higher current-carrying capacity. The most common design for Nb-Ti magnets is the Rutherford cable, which consists of two parallel flat layers of strands. Using this approach, high-aspect-ratio cables can be produced with as many as 46 strands (50). As was the case for the individual filaments, the strands are transposed around the cable, forming a densely packed square or rectangular cross-section spiral. The design con­sideration for Superconducting Supercollider Laboratory cable are discussed in Ref. 51. The compaction of the strand around the squared cable edges severely distorts the strand

Figure 11. For conventionally processed Nb-Ti the bulk pinning force increases in magnitude with drawing strain after the last heat treatment. The increase occurs at all fields as the precipitate size and spacing are reduced to less than a coherence length in thickness (45). The refinement of the microstructure with increas­ing strain for the same strand is shown schematically in trans­verse cross-sections with the a-Ti precipitates in black.

cross section, but the excellent mechanical properties of Nb-Ti/Cu composites combined with good strand design and advances in cabling technology have reduced cabling degradation to minimal levels (52).

MATHEMATICAL CHARACTERIZATION

The mathematical characterization is concerned with mathe­matical specification of the problem as some kind of transfor­mation, equation solving, and so on. In the case of digital circuit/system applications, the mathematical characteriza­tions include, for example, the following models: regular ex­pressions, extended regular expressions, data flow graphs, Pe­tri nets, finite state machines, Boolean functions, timed Boolean functions, and physical design models. The physical design models can only be realized in hardware. All of the other models mentioned above can be realized either in hard­ware or in software or in both.

The goal of mathematical characterizations is to provide the ability to investigate formally the problems of equiva­lence, optimization, correctness, and formal design correct from specification, by transformational methods.

Nowadays, most of the design is done automatically by electronic design automation (EDA) tools. The logic and sys­tem designers not only use the EDA tools, but also often de­sign their own tools or adapt and personalize the existing tools. That is why the problems of logic representation and mathematical characterization are unseparable from the logic design, and will be devoted here due attention.

High-Level Behavioral Specifications

Regular expressions are an example of high-level behavioral specification of a sequential circuit. They describe the input sequences accepted by a machine, output sequences gener­ated by a machine, or input-output sequences of a machine. Regular expressions are used in digital design to simplify de­scription and improve optimization of such circuits as se­quence generators or language acceptors. They use some fi­nite alphabet of symbols (letters) and the set of operations. The operations are concatenation, union, and iteration. Con­catenation Ex • E2 means subsequent occurrence of events Ex and E2. Union Ex U E2 means logical-OR of the two events. Iteration E* of event E means repetition of the event E an arbitrary finite number of times or no occurrence of this event. The simplest event is an occurrence of a single symbol. Extended regular expressions generalize Regular Expressions by adding the remaining Boolean operations. All the Boolean operators can be used in an extended regular expression. For instance, negation or Boolean product.

Petri nets are concurrent descriptions of sequential pro­cesses. They are usually converted to finite state machines or directly converted to sequential netlists. Because they are also used in concurrent system specification, verification, and software design, Petri nets are increasingly used in software – hardware codesign and to specify hardware (25).

Final Wire Drawing

The plain strain-imposed intercurling of the Nb-Ti grains that is so deleterious to barrier uniformity also results in the distortion of the a-Ti precipitates into densely folded sheets during final wire drawing. The folding process rapidly decreases the precipitate thickness and spacing and with a dependence of d16 (where d is the strand di­ameter) and increases the precipitate length per area with a dependence of d-16 as measured by Meingast et al. (5). As the microstructure is refined toward optimum size the bulk pinning force increases and the peak in the bulk pinning force moves to higher field as shown in Fig. 11 (data from Ref. 45). The Hc2 and the Tc gradually return to the values of the original single phase starting alloy as the precipitate are refined toward and below the superconducting coher­ence length, % (5). The critical current density increases as the microstructure is refined until it reaches a peak, af­ter which there is a steady decline. The peak in Jc for a monofilament or a multifilamentary strand with uniform filaments occurs at a final strain of approximately 5. If the filaments are nonuniform in cross section (sausaged), the peak occurs earlier and at a lower critical current density. A strand that has a premature (and lowered) peak in Jc during final drawing is described as extrinsically limited because it has not attained the intrinsic critical current of the microstructure. The most common source of extrinsic limitation is sausaging of the filaments due to intermetallic formation or lack of bonding between the components of the composite. The degree to which a composite has been ex­trinsically limited can be observed by examining the sharp­ness of the resistive transition when measuring the critical current, Ic. Volker (46) showed that the shape of the tran­sition curve near its onset can be approximated by

where V is the voltage across, I is the current in the su­perconductor, and n is the resistive transition index. For a nonextrinsically limited superconductor the value of n at 5 T, 4.2 K, can be 70 or higher. By quantifying the varia­tion in filament cross-sectional area by image analysis, the amount of filament sausaging can be measured directly (47). A high critical current density superconductor with a high n-value is shown in Fig. 12. The strand is one of a number of high-performance wires developed for the su­perconducting supercollider (48). The filament sausaging in this strand has been reduced to a very low level (a co­efficient of variation for the filament cross-sectional areas of approximately 2%). With tight quality control, uniform properties and piece lengths exceeding 10 km should be expected.

The specific pinning force for the a-Ti precipitates falls from 360 N/m2 for an average sheet thickness of 2.6 nm, to 200 N/m2 for a 1 nm average sheet thickness (14, 49) but this is more than compensated for by the increase in precipitate density caused by the continued folding of the a-Ti sheets.