Wireless Laser Power Transmission: A Review of Recent Progress

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Wireless Laser Power Transmission: A Review of Recent Progress

Wireless Laser Power Transmission: A Review of Recent Progress

1Baranika,2Akalya,3Shanthi

Mr. C. Balaji A P (EEE) Department of EEE,

Kings college of Engineering, Punalkulam, Thanjavur.

Abstract Laser power transmission (LPT) is one of the most promising technologies in the long-range wireless power transfer field. LPT research has been driven by the desire to remotely power unmanned aerial vehicles (UAVs), satellites and other mobile electric facilities. However, the low overall efficiency is the main issue that limits the implement of high intensity laser power beam (HILPB) system. As seen from the contemporary understanding of efficiency of laser power transmission channel, the efficiencies of laser and PV array are the main limiting factors to the HILPB system from the perspective of power conversion. Thus, a comprehensive overview of LPT technology is presented from the point of efficiency optimization view in this paper. First, the basic principles of laser power transmission are briefly summarized. Then, a survey of the efficiency optimization methods for HILPB system with regard to the laser and PV technologies is provided in detail. Additionally, the open issues and challenges in implementing the LPT technology are discussed.

Index TermsLaser, photovoltaic (PV), Gaussian beam, Optical propagation, Efficiency, Wireless power transmission

  1. INTRODUCTION

    IRELESS power transfer (WPT) is the technology that the electrical energy is transmitted from a power source to an electrical load without any electrical or physical connections. Compared to traditional power transfer with cord, wireless power transfer introduces many benefits such as better operational flexibility, user friendliness and product durability. Therefore, WPT technology is ideal in applications where conventional conduction wires are prohibitively inconvenient, expensive, hazardous or impossible [1]. Nowadays, WPT technology is attracting more and more attention and evolving from theories toward commercial products, from low-power smartphones to high-power electric vehicles, and the wireless powered products will come to a 15 billion market by 2020 [2].

    The development of WPT technology is advancing toward two major directions, i.e., near-field techniques, which ave a typical transmission distance from a few millimeters to a few meters, and far-field techniques, where the coverage is greater or equal to a typical personal area network.

    The former consists of two techniques: capacitive power transfer (CPT) [3], and inductive power transfer (IPT) [4- With the near-field wireless power technology reaching a mature stage for domestic and industrial applications, far-

    5], while the latter can be further sorted into microwave power transfer (MPT) [6] and laser power transfer (LPT) [7]. The key advantages of CPT are high power transfer up to several kilowatts,Transferr power through metal objectss without generating significant edddy currents losses,Use metal plates to transfer power to reduce cost, Suitable for small size application and can be used in large size applications such as EV. The potential disadvatages of CPT are limited efficiency at the range of 70%-80% but it can reach 90%in some applications, Short transmission distance which is usually within the hundered of mm range, The challenge comes ffrom the conflict amog the transfer distance and power as well as the capacitance value.The advantages of IPT are High efficiency which higher than 90% is possible, High powerr transfer upto several killowatts, Good galvanic isolation, Suitable for applications that from low power smartphones to high power EV. The potential disadvantages of IPT are Limited transmission distance with vary from cm to m, the significant eddy current loss is generated in nearby metals which limits its application area. The key advantages of MPT are long effective transmission distance upto several km, suitable for mobile applications, potential to transfer several killowatts power. The potential disadvantages are low efficiency less than 10% for high power applications(such as transfer several kw power or more), complex implementation. The key advantages of LPT are long efffective transission distance upto several km, flexible device, suitable for mobile applications, potential to transfer several kw power . The potential disadvantages are low efficiency around 20% or less, line to sight to the receiver.

    To date, both of the CPT and IPT can offer the capability of supporting high power transfer above kilowatt level with high efficiency in close distance [8-9]. However, the transferred power of these technologies attenuates quickly with the increase of the transmission range. Thus the power transfer distance is largely limited. Because of the ease and low-cost of implementation, these near field WPT technologies have found niche applications in everyday life, such as wireless charging of consumer electronics, electric vehicles (EV), robot manipulation and biomedical implanted devices.

    field wireless power research has been gathering momentum in the last decade. Both the microwave and

    laser power transfer have the ability to transfer several kilowatts power over long distance up to several kilometers, which are more flexible than those near-field wireless power technologies. Despite the common advantage of long transmission range, the lasers efficient atmospheric propagation window and its ability to deliver large amounts of power to a small aperture separate it from the microwave technology and make it an enabling technology to extend the capabilities of existing applications and facilitate the development for completely new paradigms [10]. Benefits from the advancement of the laser and PV technologies, nowadays, the high intensity laser power beaming (HILPB) system has the capability to deliver energy indefinitely to remote mobile electronic devices, such as unmanned aerial vehicles (UAVs) [10], robots [11], and orbiting satellites [12]. Moreover, it is considered to have the potential to connect lunar habitats, landing sites and power-plant and can be easily reconfigured to serve as a flexible virtual power grid [13]. The vast application potential makes the pursuit of the HILPB system a worthwhile endeavor so that the full potential of the WPT will be realized in the near future.

    A. EXISTING PROCESS:

    The concept of LPT technology is based on the principle of photoelectric effect and has been proposed since 1965 [14]. However, the development of a practical HILPB system was slow at that time due to the low efficiencies of the system components. It is until the 2000s, a variety of valued researches and applications for LPT technology have been identified and assessed. One such work is the demonstration of laser powered mini- rover that conducted by EADS Space Transportation facility in 2002 [15]. This is considered as a first step towards the use of LPT technology for powering mobile electric devices. The demonstration was based on a Nd:YAG laser at 532nm with an output power of 5W, and the power required by the rover was about 1W. A tracking system was developed to maintain an orthogonal angle between the PV cell panel and the laser beam over a distance up to 280 m.

    Later on, the first successful demonstration of laser powered aircraft flight was performed by NASA in 2003 [10]. The aircraft was fitted with a custom thin film PV array, and an adjustable 1.5kW diode array at 940nm with 50% efficiency was chosen. The 500W laser power beam was manually tracked

    the aircrafts flight path at 15mrange, resulting in a laser power of 40W to the PV array and 7W of power to the motor to sustain flight for 15 minutes. In this experiment, the beam spot size was rather large compared with that of the PV array and this was thought the main factor limiting the power transmission efficiency rather than the losses in the laser and PV cells.

    Then, in 2006, the Kinki University had successfully applied the LPT technology to the small aircraft [11]. The laser power of 300W from a laser diode transmitter was used and the power converted by the 25% efficient GaAs PV array was about 40W. The long time flight of the aircraft flying at an altitude of 50m for more than 1 hour

    with auto-tracking system had been demonstrated, which validated the feasibility of lase power transmission to an aircraft for a long time.

    After that, LaserMotive Inc. further advanced the LPT technology by demonstrating a HILPB system to power a robotic climber to a height of 1km in 2009 NASA Centennial Challenges [16]. It was confirmed that over 1kW optical power was transferred to a receiver with the overall efficiency more than 10%. In 2012, Lockheed Martin and LaserMotive, Inc. had conducted a series of proof-of-concept tests on the Stalker UAV to further validate the performance of an innovative laser power system. The demonstrations showed that the flight time of Stalker could be increased by 24 times using the laser power system. Although LaserMotive Inc. has made great progress in

    the field of LPT technology, relevant technical details have not been published yet [17].

    Recently, Beijing Institute of Technology had demonstrated a laser power transmission system at 100m based on an optimized photovoltaic (PV) converter in 2014 [18]. The system output power was 9.7W and the overall efficiency was 11.6%. In addition, in 2016, Russias Rocket and Space Corporation had successfully charged a cell phone across 1.5 km using a laser and a 60% efficient photoelectric converter. Such LPT technology will be applied to supply fuel to state-of-the-art satellites and military vehicles according to the Russian Academy of Cosmonautics [19].

    The LPT technology is still under development, most of the HILPB systems only can transmit several tens of watts across several hundred meters with relatively low efficiency and is far from its practical implementation. In order for HILPB system to become a viable option for practical wireless power transfer, each component of the system must be ensure sufficient high efficiency to provide for a high end-to-end system efficiency. Thus, most existing literatures presented relevant researches on LPT technology mainly from the perspective of device-level techniques and hardware implementations. In [22-24], the candidate laser technologies for laser power transmission are summarized from the aspect of power level, wavelength, and electro-optical efficiency. Reference [16, 25-26] focused on the performance of the PV receiver of the HILPB system. In order to achieve high optical-electro efficiency under HILPB conditions, different types of PV cells and array structures are investigated. Motivated by the numerous publications in the field of HILPB technology and by an immense amount of their real-world residential and industrial deployments, the main aim of this paper is to provide a comprehensive survey of the HILPB system with regard to the laser and PV technologies from the efficiency point of view.

    In this paper, a typical configuration of the HILPB system is presented and the basic principles of laser power transmission are briefly summarized in Section II. Then, in Section III the present enabling technologies for HILPB are provided, in order to make the best use of laser and PV array in the system, so that the system efficiency can be further improved. First, the current status of laser

    technology for high power long distance laser transmission is described from the perspective of power conversion. Furthermore, the efficiency optimization methods for PV receiver under Gaussian laser beam condition are introduced. Finally, the future research trends and concluding remarks can be found in Section IV and V, respectively.

    PROPOSED METHODOLOGY:

    Fig 1: Schematic diagram of a HILPB system.

  2. BASIC PRINCIPLES OF LASER POWER TRANSMISSION

    A. HILPB System Architecture

    Fig. 1 schematically shows a block diagram of the HILPB system [10]. As seen, the transmitter of the system converts power from a common source (battery, generator, or grid) into a monochromatic beam of light via a laser. This laser beam is then shaped with a set of optics, and directed via a beam director to the remote PV receiver. While in the receiver, specialized PV cells matched to the laser wavelength and beam intensity convert the laser light back into electricity to be used to charge a battery, run a motor, or do other work. In many ways, the HILPB system can be viewed as a kind of extension cord, with electrical power going in at one end, and electrical power coming out at the other end.

    Ideally, a HILPB system would have the ability to transmit any amount of power to any point in space, but practical limitations such as conversion efficiencies at the source and the receiver limit the performance of an implemented system [10]. Therefore, the end-to-end system efficiency must be considered in order to make a fair assessment, when considering the feasibility of a HILPB system in a particular application. Since each component contributes to the overall system efficiency, the use of high performance components is fundamental to developing a successful system.

  3. OPTIMAL PV ARRAY CONFIGURATION

As mentioned above, the efficiencies of the laser and PV array impose more severe effect on the performance of a HILPB system than that of power converters, so that improving their efficiency is strongly required. In this section, in order to make the best use of laser and PV array in the system, the methods that can be employed to

optimize the efficiency of the laser and PV array are summarized from the perspective of power conversion.

A. Efficiency Optimization Method for LD:

Fig 2: Electrical characteristics of LD.

1) The Methods to Improve the Efficiency of the LD: As mentioned above, LD is a core component in the system. It is well known that the LD is a current driven device. Thus, the input current has an apparent effect on the output of the LD. The relationship between input current i and output

of the LD. The relationship between input current i and output optical power po of an LD can be expressed by the following equation

po= d(i-Ith)

Here, d is the differential slope efficiency, and Ith is the threshold current. For simplicity, both of them are supposed to be constant. As the voltage across the LDs terminals varies little with the change of the input current, thus a constant value VLD_in can be used. The conversion efficiency can be described by using:

= po/pin=d(i-Ith)/VLD-in i= d/ VLD-in(1- Ith/i)

where po is the input power of LD. Fig. 4 shows the typical

electrical characteristics of LD. As can be seen, at above the threshold current, the optical power increases dramatically with the input current and keeps a linear relationship with the current. Furthermore, the conversion efficiency is increased along with the rising input current, and the growth rate of efficiency will slow down when input current comes to a certain extent if the temperature effect of the LD is ignored. In most practical WPT applications, the power rating of LD needs to be over- designed to cope with atmospheric absorption. Hence, the LD doesnt have to keep running at full power all the time under rated condition (eg. the operating region of the LD falls in the yellow areas of Fig. 2). This offers the advantages of lowering thermal stress to the LD and thus increasing lifetime, though the cost is increased.

In general, the LD can operate in continuous wave (CW) mode or pulse mode for the purpoe of.

Fig 3:Switching power supply with active ripple filter for LD

wireless power transmission according to the types of the input current. As shown in Fig. 4, it is assumed that the point A is the operating point of LD in CW mode. While, in order to output the same average optical power, the operating point of LD in pulse mode can be located at point B during the interval 0<t<t0. It is obvious that driving LD in pulse mode has higher efficiency at this moment However, during the interval t0<t<Ts, no light output in pulse mode and thus the efficiency of LD in pulse mode is lower than that in CW mode. So it can be seen that with the same optical output power, the operating points of LD which in different modes are different, and this could leads to the efficiency difference in different mode.

Based on the above observation, the study in [36] points out that driving LD with a pulse current gives better performance. Fig. 5 shows the experimental results of the variation of the LD efficiency in CW and pulse mode. Here, D is the duty cycle of the pulse laser, and D=1 represents continuous wave laser. As shown, by the same output optical power, the smaller the duty cycle of the pulse laser, the higher efficiency will be achieved.

Thus, driving LD in pulse mode is recommended and it can offer a chance to exploit the best performance of the LD. Moreover, it indicates that driving LD in pulse mode may give a chance for the system to further improve the operation efficiency in practice, if the whole system operates in pulse mode. The more detailed analysis can be found in [36].

2) LD driver: The LD driver is also a major component in the HILPB system, whose performance directly affects the output characteristics of LD. As well known, LD should be powered by a current source, and the main issue of the LD driver is to provide a driving current with extremely low ripple (usually lower than few tens of milliamps) for the best light output performance.

In order to do so, the typical LD power supply usually consists of a linear current regulator, as shown in Fig. 6. However, the linear current regulator has such disadvantages as low efficiency and bulky volume in high power applications. The switching mode LD driver is an alternative to the traditional linear power supply. The switching mode LD driver based on a buck type converter with a high order passive filter at output is the most common topology for generating current with a low ripple, as shown in Fig. 7 [37]. However, this approach has such disadvantages as it offers a heavy, bulky solution, and it leads to worse dynamic response. Another attractive option is to employ a typical interleaved multi-phase buck converter [38]. However, the ability of the interleaved converter to cancel the current

ripple depends on the duty cycle.

To further reduce the size and weight of the LD driver while maintain low current ripple, some active ripple filter topologies have been proposed in [39, 40]. In general, the active ripple filters have two types, which are feedforward filter and feedback filter. The feedforward filter achieves the ripple reduction by measuring a ripple component and injecting its inverse, as shown in Fig. 8(a). While the feedback filter, which is shown in Fig. 8(b), works by sensing the ripple current at the output of the filter and driving it towards to zero via high-gain feedback control.

As stated above, driving LD in the pulse mode gives a better performance, so that it is necessary to develop pulsed power supply for LD. Here, three different types are discussed, and the performance comparison of these types is shown in TABLE VI.

In the first type, a buck converter in series with a switching transistor array Q is proposed to provide pulse current to LD, as shown in Fig. 9(a)

The buck converter generates a dc current, and the transistor array Q switches the dc current to either LD or the shunt resistor. If LD is on, the dc current is sent to LD, otherwise, the dc current is sent to the shunt resistor and the input current of LD is zero. Although high dynamics is achieved, the power that sent to the shunt resistor is sacrificed.

In the second type, a bidirectional converter in parallel with a DC-DC converter, which based on the concept of active power decoupling method, is proposed to provide pulse current for LD [36]. The DC-DC converter employs average current control, with the objective of providing the average output current to the LD during the operation. The bidirectional converter is employed as the storage unit to generate the ac component of the output current. As seen, the capacitor Cb of the bidirectional converter can be reduced by increasing the voltage on it. Thus there exist theoretically possibilities to reduce the volume and weight of the storage capacitors and increase the power density.

In the third type, a single-stage pulsed power supply, which does not use any linear regulator, is proposed in [42]. Its circuit diagram is illustrated in Fig. 10. As seen, this pulsed power supply is based on a two-transistor forward converter, and a third order passive filter is used at the output of the converter to attenuate the ripple of LD current. The peak current control driven by a weighted

pulsed reference is employed to control the converter. The weighting factor k is used to adjust the average value of pulsed LD current. Since linear regulator stages and/or auxiliary components are not included, high power conversion efficiency is achieved

B. Efficiency Optimization Method for PV Array

  1. The Effects of the Gaussian Laser Beam: In practice, the flat plate array is one of the most common PV receivers for HILPB system. Since the Gaussian distribution of the laser beam, significant power losses would happen in the receiver. Thus, the efficiency of the PV array could be much less than that of PV cell under Gaussian beam condition, as shown in TABLE I. Thus, it is indicated that the high efficient PV cell cannot be made the best of using. The key reason that causes the effects of the Gaussian laser beam is the current mismatch for each PV cell in a series string [43]. Since the PV array is mismatched, some undesirable effects such as reduction in generated power and hot pots are occurred. Although bypass diode are used to avoid hot pot damage, the power-voltage (P-V) characteristics of the PV array get more complex with multiple peaks. The presence of multiple peaks reduces the effectiveness of the conventional MPPT technologies, and leading to the PV array becomes less efficient.

  2. The Methods to Improve the Efficiency of the PV Array under Gaussian Beam Condition: To mitigate the effects of the non-uniform irradiance, there are four main approaches that have been proposed.

    1. Global MPPT techniques: The first approach includes modified MPPT techniques that properly

      Fig 4: The schematic diagram of the Fibonacci search method.

      detect the global maximum power point (GMPP), and these global MPPT (GMPPT) techniques can be categorized into three groups.

      function p(v) which describes the relationship of the PV array power and voltage. For the uniformly bounded power function p(v) on the voltage interval [a, b], (4) is deduced

      P(v)max(p(v))p(v1)+M (b-a)/2

      where v1 is the sampling point which is at the center of [a, b], v is a variable and M is a Lipschitz constant. It can be seen that (4) gives a bound on how far the GMPP is deviated from the observed sample p(v1). Both M and (b-a) might be large initially. However, by taking further iterations, the voltage searching range (b-a) can be replaced by a smaller length of searching range successively. In each iteration, the searching range [a, b] is divided into three equal subintervals. Among which, the interval j is considered as the potentially optimal searching range if the following inequalities are satisfied

      p(vj)+k(bj-aj)/2p(vi)=k(bi-ai)/2,for any i p(cj)+ k(bj-aj)/2pmax+ pmax

      where Pmax is the current tracked maximumpower, and k are positive constant values. ai, bi, aj, and bj are the end points of the ith and jth intervals,

      Fig 5: MPT in the p-V plane

      respectively. P(ci) is the sampling power that taken at the center of the ith interval. The inequality (5) choses the new searching range, which has the highest potential for the maximum power, for further exploration. The inequality

      (6) ensures that the new searching range would yield further improvement than Pmax by at least |Pmax|.

      In [45], the Fibonacci search method, which is similar to the P&O method, is proposed. The

      Fibonacci search method iteratively restricts and shifts the searching range until the GMPP falls in the searching range. The process of restricting and shifting is illustrated in Fig. 11. First, the direction of the search shifting is decided based on the following rule:

      In the first group, several GMPPT methods are

      if p(v1 2

      1 2 1 2

      i) <p(v i), Then[x i+1,x i+1]=[v i,x i]

      proposed including the diving rectangle (DIRECT) method

      if p(v1 2

      1 2 1 2

      [44], Fibonacci method [45], maximum power trapezium (MPT) method [46] and I-V curve approximation method [47]. In these methods, a relatively large voltage searching range is initially

      selected. Then, the searching range is gradually reduced until the GMPP is finally located. These techniques are relatively simple and easy to implement. They can fast track the GMPP with acceptable accuracy.

      The DIRECT technique is basically a perturbation and observation (P&O) algorithm that its voltage search range are determined based on the Lipschitz condition of the

      i) >p(v i), Then[x i+1,x i+1]=[x i,v i]

      where x1 and x2 are the bounds of the searching range, v1 and v2 are the two check points in the range, the subscript i represents the iteration number, p(v1i) (p(v2i)) is the sampling voltage at the check point v1 (v1) in ith iteration. Then, in each iteration, the size of the searching range is determined by the Fibonacci sequence, such as:

      ai/bi=cn+1/cn ai+1/bi+1=ci/cn-1

      where ai represents the distance between the check point v1

      (v2) and the interval bounds x1 (x2). bi represents the

      distance between the two check points v1 and v2. cn-1, cn, cn+1 are defined in the following manner:

      co=0, ci=0 cn=cn-2+cn-1,n2

      As the experimental results that shown in [45], the

      Fibonacci search method can quickly find the GMPP by doing a wide range search, but it may mistakenly detect the local maximum power point (LMPP) instead of the actual GMPP if there are many local MPPs in the P-V curve.

      In [46], the MPT method is a modified P&O method which utilizes the knowledge of the MPT (a trapezoidal area in the P-V plane) to reduce the voltage searching range. It is reported that the trapezoidal area, as shown in Fig. 12, contains all

      Fig 6: A simple PV string under non uniform illumination

      possible GMPPs for any non-uniform irradiance conditions. As seen, the trapezoidal area is limited to the right by a vertical segment at 0.9Voc,STC,array and limited to the left by a segment in the origin with a slope of IGMPP,STC,array (array GMPP current at STC). During the process of tracking GMPP, the upper bound of the voltage searching range is fixed at Vrange,max

      =0.9Voc,STC,array (open circuit voltage of the array at STC).

      During the process of tracking GMPP, the upper bound of the voltage searching range is fixed at Vrange,max

      =0.9Voc,STC,array (open circuit voltage of the array at STC). The lower bound of the voltage searching range is determined by

      Vrange,min= Pmax/IGMPPSTC,array

      where Pmax is the current tracked maximum power. As seen, the lower bound Vrange,min increases along with the increase of the detected Pmax. Therefore, since Vrange,min increases in each iteration and Vrange,max is fixed, the voltage searching range is gradually reduced until the GMPP is reached. The I-V curve approximation method proposed in [47] can narrows the searching window and tracks the GMPP very fast. First, it takes some samples from the PV array and divides the voltage searching range into small subregions. Then, the method approximates the I-V curve in each subregion with a simple curve, as shown in Fig. 13. As seen, an upper limit Pup-k for the array power in subregion k [Vk, Vk+1] can be set as:

      Pup-k=Vk+1×Ik

      where Ik is the current of the sample K. Obviously, the GMPP is not in that subregion whose upper limit Pup-k is lower than the maximum value of all measured powers Pmax and this subregion can be eliminated from the searching range. Therefore, by comparing the Pmax with the estimated up limits, the searching range is limited.

      Hereafter, with similar procedure and further intelligent samplings, the searching range becomes smaller gradually until the vicinity of GMPP is achieved.

      The second group is the GMPPT methods that utilize the unique characteristics of the IV or PV curve of the PV array under non-uniform irradiance conditions to track all the LMPPs or move operation point to the neighborhood of GMPP. Then, the conventional P&O or IncCond method can be adopted to attain the GMPP. Some examples of these methods are summarized as follows.

      The load-line method, which is proposed in [48], utilizes the load line to bring the operating point into the vicinity of the global maximum. The function of the load line is defined as

      I=(Impp/Vmpp)V=(0.8Voc/0.9Isc)V

      where Impp, Vmpp, Voc and Isc is the current of the MPP, voltage of the MPP, open circuit voltage and short circuit current of the array under uniform irradiance conditions, respectively. When the non-uniform irradiance occurs, it is claimed that the operating point is moved to the neighborhood of GMPP, which is the result of intersection of the load line with the I-V curve of the PV array. Then, the conventional MPPT methods are used to find the GMPP. It can be seen that the load-line method is simple and can achieve fast tracking speed, but the tracking result may be one of the local MPPs rather than the GMPP.

      In order to improve the tracking accuracy, the power increment method is proposed in [49]. In this method, the searching process starting from the open circuit condition, the power converter which connected to the PV array is controlled as an adjustable power load and the power that drawn from the PV array is increased at each step, resulting in the operation point moving toward to GMPP. Once the drawn power cannot be further increased, the power increment process is stopped and the power converter controls the operation point back to the last detected point. Therefore, the neighborhood of GMPP is determined. Then, the conventional MPPT methods can be adopted to attain the GMPP. As the experimental results that shown in [49], the difference between the tracked GMPP and the actual GMPP is less than 0.1%. However, as the power increment method needs to search a large range of voltage, so that the tracking speed of the power increment method is slower than that of the load-line method.

      In [50], a simple GMPPT method, referred to here as ramp voltage scanning method, is proposed. By observing the IV and PV characteristics of PV array, it is worthy to note that the positions of all peaks in PV curve (includes the GMPP of the array) stay at the following voltage range under non-uniform irradiance conditions:

      Vmpp-mod<V<0.9Vopen

      where Vmpp-mod is the voltage of the module at its MPP, and Voc-arr is the open circuit voltage of the array under non-uniform irradiance conditions. To scan the restricted voltage range, this method using the ramp voltage command (instead of conventional step-like changes) as the voltage reference of the converter which connected to the PV array and simultaneous sampling the voltage and current of the array continuously. In this method, due to the

      oscillation of array voltage can be avoided, the long delays in usual methods for correct sampling of voltage and current are nt needed any more. However, it searches almost all the range of PV curve and thus, its tracking speed is still not good enough.

      The 0.8Vocmodmodel method, which is proposed in [51- 54], is based on the conclusion that the peaks of a PV curve under non-uniform irradiance conditions occur nearly at multiples of 80% of modules open circuit voltage Vocmod. In [51], the proposed method first samples the PV curve in distances of 0.8Vocmod. Then, in the vicinity of each sample, the conventional P&O method is used to track the local peak in case of sign change of dP/dV. Finally, by comparing all peaks, the GMPP is determined. Even though the 0.8Vocmodmodel method only needs to search the vicinity of the 0.8Vocmod regions rather than the entire P-V curve, the tracking speed of this method is generally slow for long PV string applications because each peak must be searched by the P&O method. On the other hand, the reference [52] points out that the peaks of PV curve are located at the multiples of 0.8Vocmod which is not always true, especially for long PV strings. Therefore, the 0.8Vocmodmodel method may lead to incorrect GMPP detection. The further study about the 0.8Vocmodmodel method is presented in [53]. In [53], it is claimed that the value of the minimum voltage interval between the MPPs varies in a wide range starting from 0.5Vocmod. Thus, the proposed method in [53] uses the voltage step of 0.5Vocmod to scan the PV curve for GMPP. However, this method may not find GMPP in scanning with step of 0.5Vocmod in some cases [54].

      The R-GMPPT method, which is a modified 0.8Vocmod model method, is proposed in [55]. In [55], it is stated that for an n PV modules connected in series under non-uniform irradiance conditions, the P-V curve shows n divide intervals, and every interval has one peak power points (PPPs). The voltage and current of the jth (j=1, 2,

      , n) PPP, ie., Vmj and Imj can be expressed as:

      Imj0.9Iscj

      Vmj(j-1)Voc-mod+0.76Voc-mod=(j-1+0.76)Voc/n

      where Iscj is the short circuit current of the jth PV module, Voc and Vocmod is the open circuit voltage of the PV string and module, respectively. A simple PV string is used as example to make the concept of the above formulas clearer, as shown in Fig. 14. As seen, A and B are the PPPs of this string. On the left of point M, only PV1 works, It is well known that the current of PPP A is approximately equal to 0.9Isc1 (short circuit current of PV1), and the voltage of PPP A is approximately equal to 0.76Voc1 (open circuit voltage of PV1). On the right of point M, PV1 and PV2 works, but the I-V curve is mainly affected by PV2. Thus, the current of PPP B is approximately equal to 0.9Isc2, and the voltage of PPP B is approximately equal to sum of Voc1 and 0.76Voc2. For simplicity, Voc1 and Voc2 can be considered equal to Vocmod, which is equal to half of the open circuit voltage of the PV string Voc. Thats is, Vm1=0.76Voc/2 and Vm1=(1+0.76)Voc/2.

      According to (14) and (15), the approximate power of all PPPs can be calculated as:

      PmjVmjImj(j-0.24)Voc×0.9Iscj/n

      With the maximum value in these calculated Pmj, the neighborhood of GMPP can be determined. Then the P&O method is used to track the GMPP. As reported in [55], the R-GMPPT method can reduce more than 90% of the tracking time that is consumed by the conventional global searching method, while maintains acceptable tracking accuracy.

      Similar to the concept of R-GMPPT method, the proposed IV curve mapping method in [56] maps out the pattern of IV curve under non-uniform irradiance conditions by sampling the array current. Based on the analysis of the step-like IV curve under non-uniform irradiance conditions, it is shown that the current in each step of the I V curve is almost constant up to the end of that step. Moreover, the starting points of each step are in near left side neighborhood of the multiples of modules open circuit voltage Vocmod. According to the above observation, this method samples the array current in multiples of Vocmod and compares these sampling currents against each other. As a result, the number and length of IV curves steps are determined. Then, based on the mapping, the hill climbing algorithm is called to search the vicinity of the multiples of 0.8Vocmod to track all MPPs. Finally, by comparing the value of tracked MPPs, GMPP is determined. A similar method is proposed in [57], this method can map out the locations of all LMPPs by measuring the voltages of every PV modules and calculates the appropriate reference voltage to track the GMPP around it. Obviously, compared with the method in [57], the IV curve mapping method is simple to implement. Because the IV curve mapping method only needs just one current sensor to track GMPPT, while the method in [57] uses one current sensor for each PV module.

      The third group includes some intelligent algorithms, such as particle swarm optimization [58], artificial bee colony [59], and fuzzy-logic control [60]. The advantages of intelligent algorithms are their adaptive ability of accurately tracking GMPP regardless of the condition of illumination and the configuration of the PV array. However, the intelligent algorithms are complex to implement, and the initial point must be carefully selected by professionals.

      The development of GMPPT techniques is more attractive due to simplicity of implementation, reduced cost, and the immediate adoption to existing system. TABLE VII provides the performance comparison of the GMPPT methods that mentioned above. A more detailed review on the GMPPT techniques can be found in [61]. Note that, although it can harvest more energy by utilizing the global MPPT techniques, it has no effect on the power loss caused by the Gaussian beam.

    2. Modified PV receiver geometries: The second category to maximize the efficiency of the PV array would be employing different modified PV receiver geometries.

      In [12], the radial orientation array is proposed. By placing the PV cells on a radial to the center-point of the receiver or adjusting the manufacturing of the cells to obtain an optimal radial geometry that reflects the Gaussian distribution of the laser beam, an equal average illumination per cell can be achieved for the series

      connected PV cells in each annular area. In this way, the uniformity of the junction illumination can be improved. However, the geometrical loss, complicated structure and high cost are major issues that limit the implementation of the radial orientation array.

      On the other hand, a sawtooth-configured array in which the PV cells are angled is proposed in [52]. With the angled PV cells, the irradiance at each point is reduced by a reduction factor. The reduction factor is a function of a cosine of the angle of the incident beam. The closer to the center of the array, the bigger the angle and the more laser power is reflected. Therefore, with this surface geometry arrangement, all cells in the array substantially can receive the same irradiance. However, the reflected laser beam which caused by the angle of each cell could significantly reduce the power transfer to the PV cell, and it is an obstacle for the efficiency improvement of the PV receiver. In [21], a complicated PV receiver, which is named Photovoltaic Cavity Converter (PVCC), is proposed. The back-scattered light illuminates the cavity uniformly, so that the effects of the non-uniform irradiance can be avoided. Benefit from photon re-cycling in the cavity, the PVCC has the potential to convert high density laser to electricity at unprecedented efficiency. However, the current PVCC prototype functioning within the 100W to 200W laser power level only has a efficiency of 14%. It has been analytically shown that an array conversion efficiency of over 60% can be achieved if cells with perfectly matching band-gaps are used as well as the flux density inside of the sphere and the cell population density within the PVCC are increased. Its worth pointing out that, at that such small aperture on the cavit, the high pointing accuracy is required.

    3. Array configuration: An alternate approach is one that employs different PV array configurations for interconnecting PV cells or modules, which are typically either series-parallel (SP) or total-cross-tied (TCT) configurations [63, 64]. Obviously, the actual electrical connections of PV cells in the PV array are different for different configurations, resulting in different GMPPs under the same Gaussian beam condition. In order to improve the performance of the PV array to counter Gaussian laser beam, the PV array configuration needs to appropriate design according to the energy distribution of the laser beam. As the TCT and SP configurations are widely used in practice, thus these two configurations are discussed here, in order to explore their performance under Gaussian beam condition.

In [20], the SP array is employed and the interconnection scheme is designed to minimize the impact of beam non- uniformity using the energy distribution of the laser beam. Thus, the irradiances on the PV cells which in the same string are closed to each other, so that the maximum power of each string can be improved. The measured efficiency of this SP array was 21.9% under a laser beam at 0.3 W/cm2. However, this was less than half the expected efficiency due to the beam non-uniformity.

In [65], it is found that the interconnections between the PV strings are able to balance the irradiance across each tier in the TCT structure. This may decrease the current

that flows through the mismatched cells, thus blocking the operation of bypass diodes. Therefore, compared with the traditional SP array structure, the TCT structure can improve the MPP of the PV array under non-uniform irradiance conditions. In [66] and [67], the experimental results show that the TCT configuration can improve the amount of maximum power by 5.84% and 3.8% compared with the SP configuration under different non-uniform illumination conditions, respectively.

Fig 7: Different configuration of PV array

Fig 8: The reconfigurable PV array

Obviously, for the TCT configuration, swapping the cells from one position to another can obtain different MPPs. For optimal performance, the PV cells in the TCT configuration need to interconnect in an irradiance equalization manner, so that the total irradiance (and therefore current producing ability) at each tier is almost equal.

In many literatures, different reconfigurable PV arrays are proposed to cope with the Gaussian beam condition. For example, a reconfigurable TCT PV array is developed in [68]. The switching matrix, which connects the fixed and adaptive part, is used to recombine the individual PV cells in the array under non-uniform illumination conditions. The switching matrix is controlled by an adaptive reconfiguration algorithm to automatically connect the most illuminated PV cells in the adaptive bank to the least illuminated row of the fixed part, so that each PV modules composed by the PV array operating under similar irradiance conditions. As reported in [68], for a 3×3 TCT PV array with a 3×1 adaptive part, there is a 65% increase in output power from before to after the reconfiguration.

Another reconfigurable PV arrays with TCT configuration, which is named dynamic photovoltaic arrays (DPVAs), is developed in [69] to cope with the effects of non-uniform irradiance. As shown in Fig. 17, the biggest advantage of the DPVAs is that the dimensions of the PV array can be arbitrary resized and all possible connection schemes are available in practice. As proposed in [69], the best connection scheme of DPVA is determined by the irradiance equalization algorithm. This irradiance

equalization algorithm is essentially an iterative and hierarchical sorting

Thus, instead of developing a real-time algorithm and the flowchart of it can be found in section IV of [69]. As the irradiance equalization algorithm is based on simple sorting, flipping and adding, the searching time of it is very fast, which means the algorithm is suitable for large PV array.

As above, the reconfigurable PV array shows the most improvement of MPP compared with the static TCT configurations under the frequently changing illumination conditions. However, the reconfigurable PV array is complex. Since the Gaussian distribution of the laser beam is constant and regular, it is considered that there exists a certain optimal interconnection scheme which is able to maximize the PV array .reconfigurable PV array, it is a good option to employ a fixed configuration for arranging the cells so as to enhance the PV power generation under Gaussian beam condition.

In order to do so, an optimal configuration research algorithm for static TCT configuration is proposed in [70]. Since the output power of a PV array is related to the irradiance value of each PV cell, the irradiance across a PV array under Gaussian beam condition is simplified first in [70]. The process of simplifying the energy distribution of Gaussian laser is essentially using a step function to fit the Gaussian function. Then, according to the irradiance on every individual PV cell in the TCT array under Gaussian laser beam condition, the optimal TCT configuration search algorithm which based on the irradiance equalization method is proposed.

Fig 9: The voltage injection topology

Fig 10: The simplified model of Gaussian beam

Fig 11: Multi chopper based GCC

The main steps of this algorithm are summarized as follow: First, define and sort the irradiance of all the PV cells in the PV array in a decreasing order and converted to a PV cell bank. Then, connect the most illuminated PV cell in the PV cell bank in parallel to the module which has the smallest total irradiance. This process will continue until all the PV cells which in the PV cell bank are connected parallel to the rows of the TCT configuration.

As reported in [70], the simulation results show that there is a 33% increase in MPP power from before to after the algorithm is executed for the 3×3 TCT PV array. Moreover, the xperimental results indicate that the optimal 3×3 TCT configuration has better performance than the optimal 3×3 SP configuration with a 9.2% improvement in MPP power.

d) Power electronics equalizer: In fact, the partial shading effects in PV arrays have been widely investigated, and the effect of Gaussian beam condition for PV array is a special case of that. Thus, the concept of the power electronics equalizer that used to mitigate the partial shading effects can be borrowed to further enhance the output power of PV arrays under the Gaussian beam condition. The aim of the power electronics equalizer is to eliminate the multiple peaks, so that only one peak power point exhibited in the P-V curve under Gaussian beam condition. In general, the circuit topologies of the power electronics equalizer differ in their implementation, efficiency, number of active and passive elements, complexity

Fig 12: Topology of CCT and key waveform

of control systems, upgradability, and the capability of individual MPPT for each PV module.

Here, three different groups are discussed.

The first group, which is named voltage injection topology [71], [72], is shown in Fig. 19(a) and (b). As seen, the PV string is series connected with a dc-dc converter.

The main function of the DC-DC converter is to provide the bias voltage Vbias_i for the ith PV string, so that the GMPP of the less illuminated string can be aligned with the MPP of the highest illuminated string, resulting in more power can be extracted from the PV array, as illustrated in Fig. 19(c) and (d). This circuit topology can be upgraded by using more DCDC converters as the number of PV strings increases. However, the additional circuits increase the system complexity and cost.

The second group is the compensation circuits that are employed to improve the output power of a PV string by controlling the voltages of PV modules at its MPPs. Here, two different approaches re discussed.

In the first approach, the generation control circuit (GCC), which is based on the multi-chopper topology is proposed in [73], as shown in Fig. 20. In this topology, each unit is controlled to regulate its output voltage to ensure that all PV modules are working at their MPPs by adjusting the off-duty ratio of its switch. Although this topology has good performance in improving the output power of a PV string and can be upgraded as the number of PV modules increases, its implementation is complex for long PV string. It should be noted that the GCC scheme only makes the PV modules operate at an approximate MPP based on the assumption that the MPP voltage does not change significantly with irradiation and/or temperature. However, the MPP voltage does change with irradiation and temperature

Fig 13: Topology of PV equializer

Therefore, in the second approach, a more accurate compensation scheme is proposed in [74 In this scheme, a flyback converter is connected parallel

to each PV module. Here, the flyback converter can operate in two modes: resonant MPPT mode and normal flyback mode. First, in order to determine the MPP voltage of each module, the flyback converter is controlled to operate in resonant MPPT mode, so that the voltage of PV module begins to resonant and passes through the MPP voltage. Then, the flyback converter is controlled to operate in normal flyback mode to regulate the PV modules voltage at its desired MPP value. In the third group, several topologies based on current compensation are proposed. The output current of these circuits is used to compensate for the difference between the string current and the current of the less illuminated PV module. Here, three typical types of these circuits are reviewed.

The RECC unit is controlled as a current source to inject the correct magnitude of current into the PV.The power associated with the injection of the compensation current is taken from the output of the string. However, the desired current level in the PV string remains to be determined for the power circuit loss minimization.

As seen, each CCT unit is paralleled with a PV module, and the output terminals of these units are connected in series. Any degree of decline in the output current of less illuminated PV module (PV2) would activate the corresponding CCT to magnify the output current (i2) in order to match the PV string current (i1). To consider minimizing the power circuit loss, the CCT output current is controlled at an appropriate value by a dependent current source (DCS). Although accuracy of this method is high and it can decrease the effect of non-uniform irradiance conditions on the array power, its implementation is expensive.

In a PV equalizer, which is based on the battery voltage equalization circuit, is proposed in [77]The equalizer has three modes: equalize, bypass, and search. The equalize mode is the main function of the equalizer. It draws the excess current from the most illuminated module groups and shares it with the shaded ones. This is done through the successive charging and discharging of an inductor at high

frequency by choosing the appropriate switches to be controlled and their duty cycle.

It can be seen that the efficiency of the PV array can be improved by using the different modified MPPT methods and employing the different PV array configurations.

COMPONENTS REQUIREMENT & COST DETAILS:

Available Types of Laser :

Nowadays, there are various types of lasers. In principle, the selection of a laser for HILPB system needs

to comply with several fundamental constraints related to the: 1) the possibility to transfer the energy through the atmosphere, 2) the possibility to transfer the energy as long as possible. For the former constraint, as the atmosphere is comprised of various gases that fluctuate in composition due to environmental conditions, the atmosphere will absorb certain energies at particular wavelength. So, the lasers need to be considered must operate in the wavelength range centered around the spectrum in the window in the

TABLE 1: SUMMARY OF MAIN COMPONENTS OF VARIOUS HILPB SYSTEMS

Laser transmitter

PV receiver

Whole system

Laser type

Wavelength (nm)

laser (%)

Cell type

PV-

cell(%)

Incident energy(W/m2)

pv-

array(%)

Distance (m)

Output (W)

system(%)

Diode 1.5kW

940

50

Si

14.6

560

17

15

<8.5

Diode 400W

808

GaAs

300W

14

50

40

<14

Nd:YAG

Laser

523

InGaP

<5W

40

280

>1

Disk 8kW

1060

25

Si

35

2kW

5

103

100

1.25

Diode 25W

793

30

GaAs

6×104

40.4

100

9.7

11.6

Diode 2kW

810

GaAs

50

3×103

21.9

100

200

Nd:YAG

Laser

1060

Si

50

300

14

3

19

<14

TABLE 2: EFFICIENCIES OF DIFFERENT PV MATERIALS UNDER LASER ILLUMINATION

PV material

GaAs

Si

InGaAs/InP

InGaP

CIS

Suitable laser wave length

810nm

950nm

>1000nm

pv(%)

53.4

60

27.7

28

40.6

40

19.7

Incident laser intensity(kW/m2)

430

110

10

110

2.37

2.6

10

which the atmosphere is nearly transparent in order to maximizing energy transfer. It is reported that region between 780 and 1100 nm is particularly relevant for commonly available laser technologies that produce sufficient power for wireless power transmission [24].

Available types of PV cells : At the receiver of the HILPB system, the appropriate PV cell should be carefully designed so that the laser power can be effectively converted into electricity. In order to do so, the factors of the laser power, wavelength, temperature and the material of the PV cells should be considered.

For a PV cell, the photons must have energy greater than or equal to the band-gap in the material in order for the cell to generate electricity. Since the energy of a photon is proportional to its frequency, PV cells are responsive to particular frequencies of light corresponding to the cells band-gap energies. Thus, the ideal light source like Si and GaAs could reach the highest conversion efficiencies when illuminated with monochromatic beams of wavelengths 900nm and 850nm, respectively.

On the other hand, it is the fact that when a PV cell is illuminated with more intense light than the solar radiation, the cell not nly generates more absolute power, it is also

more efficient for a given temperature [28]. Thus, the PV cell that can provide efficient operation at high laser power intensity is more desirable.

would be monochromatic and at an ideal frequency for the PV material, instead of spread across a broad spectrum of frequencies, as sunlight is. The spectral-response curves for some different PV materials are illustrated in Fig. 2 [27]. As seen, the most widely used PV cells

TABLE IV shows estimated efficiencies under laser illumination for different PV materials. As seen from the TABLE IV, the GaAs PV cell is the highest efficient PV converter. The GaAs PV cell has greater than 50% efficiency under light of the right wavelength [29-31]. Moreover, the GaAs PV cell is best suited to wavelengths around 850 nm, which is ideal for the LDs. While, for Si PV cell, the most ideal wavelengths comes at about 900- 950nm, but atmospheric absorption is too high in this region to make Si PV cells a strong competitor [27]. The InGaAs, InGaP and CIS cells are responsive to the wavelengths of more than 1 m, which are ideal for the DPSSLs. However, these materials are not efficient enough under high illumination intensity

APPLICATION:

Wireless technology really allows a network to reach locations that could not be achieved by using a network cable. With the wireless system can provide the user with various access information in real-time anywhere. Given this extremely supportive in productivity and an increase in kualias than using a wired network. Next advantages is the ease of installation. You do not necessarily need a cable to connect two or more computers. Then the installation process it will be much easier and lighter without stalling cable or perforate the wall. A wireless LAN system can be configured with a variety of network topologies to meet the needs of the user. Himself the configuration can be changed from peer to peer with a small number of users to full infrastructure networks with up to thousands of users, and so allows for roaming in a large area.

V. CONCLUSION

In this paper, the state of the art in LPT technology is reviewed. The recent progress on laser wireless power transfer is described. Several available types of lasers and PV cells are presented. The use of commercially available LD and GaAs PV cell proved to be effective. Current laser technology and reasonable apertures can produce useful beam intensity at the receiver within a range of 10km. In the operation of the HILPB system, it can be seen that the power system met with barriers arising from beam non- uniformity, which hinder the improvement of the system efficiency and may be overcome though the use of modified MPPT methods and different PV array configurations. Moreover, the performance of the LD that operates in pulsed mode is presented, which has advantages in efficiency. Therefore, it may offer a chance to improve the operation efficiency of the system. Additionally, the open issues and challenges for future research are provided. Further research in laser wireless power transfer requires the combined efforts of the professionals and researchers in the areas of PE, control, laser, material science, and optical. The major challenge for the future is further improvements in laser wireless power transfer with better energy efficiency for a given transmission distance.

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