fig1 depicts a schematic drawing of a lidar system in accordance with the illustrative embodiment of the present invention . system 100 includes transmitter 102 , receiver 104 , and processor 106 . fig2 depicts operations of a method for developing a map of objects in a detection field in accordance with the illustrative embodiment of the present invention . method 200 begins with operation 201 , wherein transmitter 102 transmits a train of pulses 110 along detection axis 112 . transmitter 102 is an optical transmitter suitable for emitting a train of optical pulses having a wavelength within the range of approximately 1350 nm to approximately 1390 nm . typically transmitter 102 generates the optical pulses using a laser source , such as a diode laser . one skilled in the art will recognize that the performance of a lidar system is based on several factors , such as available optical power , the sensitivity of the detector used to detect reflected pulses , and the desired sensitivity of the system . the present invention employs single - photon detectors , which greatly reduces the amount of optical power required in pulses 110 . significant optical power is still required to enable a suitable signal - to - noise ratio ( snr ) for longer detection distances , however . unfortunately , the amount of optical power that can be used in a lidar system is constrained by eye - safety issues . these are particularly stringent at shorter wavelengths , such as at 905 nm , a typical operating wavelength of prior - art lidar systems . it is an aspect of the present invention that operation at a wavelength within the 1350 - 1390 nm - wavelength range enables embodiments of the present invention to take advantage of a relatively narrow intensity dip in the solar background spectrum . this wavelength range also exploits an eye - safety threshold that is more than an order of magnitude higher than at 905 nm . fig3 depicts a plot of maximum permissible energy ( mpe ) versus wavelength for pulses having different pulse widths . one skilled in the art will recognize that the mpe denotes an eye - safety threshold for the power at which a lidar system can safely operate . it is apparent from plot 300 that , for nanosecond pulse widths , mpe is approximately 1 microjoule / cm 2 at a wavelength of 900 nm ; however , it increases to approximately 50 , 5000 , and 10 6 microjoules / cm 2 at the wavelengths of 1350 , 1450 , and 1550 nm , respectively . by operating at longer wavelengths , therefore , system 100 can provide higher laser power without exceeding the eye safety threshold . it should be noted that plot 300 also suggests that operation at 1550 nm should enable even longer ranging distance , as well as improved system performance . unfortunately , the solar background radiation is also higher at 1550 nm wavelengths , thereby degrading the signal - to - noise ratio and negating many of the benefits of long - wavelength operation . fig4 depicts a plot of solar power density as a function of wavelength . while plot 400 evinces that the power level of the solar background is quite high at 1550 nm , it also shows that it dips significantly within the range of approximately 1340 nm to approximately 1500 nm . trace 402 indicates a sliding 40 nm - wide average of the solar energy . window 404 denotes a 40 nm - wide wavelength window suitable for vehicular lidar operation , which is centered at 1370 nm in accordance with the illustrative embodiment of the present invention . it should be noted that other operational windows are in accordance with the present invention . for example , plot 400 also depicts window 406 , centered at approximately 1455 nm , which represents another possible window of operation for system 100 . operation in this wavelength regime allows pulse 110 to be at a higher energy level by virtue of a higher mpe at this higher wavelength . transmitter 102 transmits each of pulses 110 such that it has a duration of approximately 5 nanoseconds at a repetition rate of approximately 300 khz . in some embodiments , each of pulses 110 is transmitted with a duration that is less than 5 ns . in some embodiments , each of pulses 110 is transmitted with a duration that is greater than 5 ns . one skilled in the art will recognize that the pulse width of pulse 110 and the repetition rate of transmitter 102 are matters of design and can that pulse 110 can have any suitable values . in the illustrative embodiment , the repetition rate of transmitter 102 is based on the desired maximum range of detection , lmax , in detection field 114 ( i . e ., the size of detection field 114 ). in the illustrative embodiment , transmitter 102 transmits a train of pulses 110 at a repetition rate of 3 . 3 microseconds , which is based on the time - of - flight for a photon travelling to and from an object that is at a maximum detection distance that is approximately 500 meters from receiver 104 . this time - of - flight also determines the duration of each of a plurality of detection frames for system 100 , as discussed below and with respect to fig5 . it should be noted that , in the illustrative embodiment , system 100 is mounted on vehicle 108 such that transmitter 102 and receiver 104 are substantially co - located . in some embodiments , transmitter 102 and receiver 104 are not co - located and are separated by some separation distance and the repetition rate of transmitter 102 is based on the total time for a photon to travel from transmitter 102 to an object located at lmax and be reflected back to receiver 104 . at operation 202 , processor 106 enables receiver 104 to detect reflection 116 . fig5 depicts a circuit diagram of a portion of a receiver in accordance with the illustrative embodiment of the present invention . receiver 104 comprises single - photon avalanche diode ( spad ) 502 and load 504 . in some embodiments , receiver 104 includes a negative - feedback avalanche diode ( nfad ), a spad operatively coupled with a switching element ( e . g ., a transistor ) operative for discharging the spad after an avalanche event , a photodiode operating in linear mode , or another suitable photodiode . spads and nfads suitable for use in the present invention are described in detail in u . s . pat . nos . 7 , 378 , 689 and 7 , 719 , 029 , each of which is incorporated herein by reference . fig6 depicts a timing diagram for receiver operation of a lidar system in accordance with the illustrative embodiment of the present invention . each detection frame depicted in timing diagram 600 ( i . e ., detection frame 602 - 1 ) begins at time to , when transmitter 102 transmits pulse 110 . at time t 1 , processor 106 arms spad 502 by applying a voltage bias , v 2 , at terminal 506 , where v 2 exceeds breakdown voltage vbr of spad 502 . for the purposes of this specification , including the appended claims , “ arming ” a spad is defined as putting the diode into geiger mode by biasing it with a bias voltage that exceeds the breakdown voltage of the spad . one skilled in the art will recognize that when armed , receipt of a single photon will give rise to an avalanche event that results in a macroscopically detectable current through the spad . in similar fashion , “ disarming ” a spad is defined taking it out of geiger mode by reducing its bias voltage below the breakdown voltage of the spad . it should be noted that time t 1 is delayed slightly from time t 0 to account for the transmission duration of pulse 110 , during which detection of reflection 116 is disabled . in some embodiments , spad 502 is armed simultaneously with , or during , the transmission of pulse 110 . prior to absorbing a photon , the entirety of vbias is developed across spad 504 since the magnitude of avalanche current , i , is zero and there is no voltage drop across load 504 . as a result , the magnitude of vout ( provided to processor 106 at terminal 508 ) is equal to zero . although the illustrative embodiment comprises a load that is a resistive load , in some embodiments of the present invention , load 504 comprises a circuit element in addition to or other than a resistor , such as a capacitor , inductor , or reactive element ( e . g ., a transistor , etc .). at operation 203 , receiver 104 detects reflection 116 , which originates from object 118 . reflection 116 is detected at receiver 104 at time tr . upon absorbing a photon , avalanche current , i , builds through spad 502 and load 504 . as a result , a voltage drop equal to i · r will appear across load 504 , where r is the resistance of load 504 . as a result , processor 106 detects a change in the magnitude of voltage vout , at time tr . at operation 204 , processor 106 computes the distance between vehicle 108 and object 118 based on the delay between times t 0 and tr . it should be noted that the use of an nfad in receiver 104 enables detection of multiple reflections within a single detection frame , since an nfad can be rapidly quenched and re - armed at rates higher than the typical repetition rate of transmitter 102 , as discussed in detail in u . s . pat . no . 7 , 719 , 029 . at operation 205 , processor 106 disarms spad 502 at time t 2 by reducing its bias voltage below vbias . it should be noted that time t 2 in detection frame 602 - 1 is also time t 0 of detection frame 602 - 2 . in some embodiments , operations 201 through 205 are performed for each of detection frames 602 - i , where i = 1 through n and n is a desired number of detection frames over which it is desired to interrogate detection field 114 along detection axis 112 . repeated interrogation of the same detection axis enables the use of statistical methods to increase system tolerance for false counts at spad 502 . in some embodiments , digital thresholding is used to increase system tolerance for false counts , as discussed below and with respect to fig7 - 10 . at operation 206 , system 100 scans detection axis 112 horizontally such that system 100 interrogates a different portion of detection field 114 . in some embodiments , system 100 scans detection axis 112 vertically . typically , detection axis 112 is scanned via a rotating element , such as a mirror , prism , and the like . in some embodiments , transmitter 102 and receiver 104 are mounted on a scanning element , such as a turntable , gimbal element , etc ., which enables detection axis 112 to be scanned . in some embodiments , system 100 includes a one - or two - dimensional array of transmitters and / or receivers that are arranged to simultaneously interrogate detection field 114 along a plurality of detection axes arranged horizontally and / or vertically . at operation 207 , processor 106 develops a map of detection field 114 . it should be noted that even when system 100 operates at a wavelength within the range of 1350 - 1390 nm , the power level of the solar background is still quite high and can lead to false counts at receiver 104 , as shown in table 1 below . although the false - count rate at 1370 nm is much lower than at other wavelengths , even at 1370 nm , 6 - 30 false counts will occur in a detection frame of approximately 3 microseconds . it is another aspect of the present invention that the negative impact of solar background on system performance is mitigated by apportioning each detection frame into a plurality of sub - gate periods . in other words , by dividing each detection frame into smaller time intervals in which spad 502 is armed , the probability of a false count during each sub - gate period can be greatly reduced , as shown in table 2 below . fig7 depicts a schematic drawing of a lidar system in accordance with a first alternative embodiment of the present invention . system 700 is analogous to system 100 ; however , in operation , processor 702 is operative for logically separating detection field 114 into detection zones 704 - 1 through 704 - 3 ( referred to , collectively , as zones 704 )— each of which corresponds to a different sub - gate period within each detection frame . in the first alternative embodiment , detection field 114 is separated into three zones ; however , it will be clear to one skilled in the art , after reading this specification , how to specify , make , and use embodiments of the present invention wherein detection field 114 is separated into any practical number of zones . fig8 depicts operations suitable for developing a map of a detection field in accordance with the first alternative embodiment of the present invention . method 800 begins with operation 801 , wherein , for each of i = 1 through n , system 700 interrogates detection field 114 along detection axis 112 during detection frame 1002 - i . n is the number of times interrogation of detection axis 112 is repeated before rotating detection axis 112 to enable system 100 to interrogate a different portion of detection field 114 . the value of n is based on a number of factors . for example , in any lidar system , it is important to be able to distinguish detection of a signal photon ( i . e ., a photon arising from reflection from an object in detection field 114 ) from a detected “ noise photon ” due to the solar background , a dark count , and the like . for proper system operation , a probability of detection ( pd ) of a signal photon is preferably at least 99 %, while the false alarm rate ( far ) due to noise photons is preferably & lt ; 1 %. it is yet another aspect of the present invention that , by interrogating detection axis 112 repeatedly to collect data from multiple detection frames , statistical methods and / or digital thresholding can be employed to increase pd and decrease far , as discussed below . fig9 depicts a sub - method suitable for interrogating a detection field along a detection axis in accordance with the first alternative embodiment of the present invention . operation 801 begins with sub - operation 901 , wherein transmitter 102 transmits pulse 110 along detection axis 112 . fig1 depicts a timing diagram for interrogating a detection field along a detection axis in accordance with the first alternative embodiment of the present invention . in similar fashion to timing diagram 600 described above and with respect to fig6 , each measurement frame 1002 - i begins at time t 0 - i , when transmitter 102 transmits pulse 110 - i . for each of j = 1 through m , where m is the number of sub - gate periods within each detection frame , processor 106 enables receiver 104 to detect a reflection that originates only within zone 704 - j . detection of a reflection originating within each zone 704 - j is enabled at sub - operation 902 , wherein spad 502 is armed at time ta - i - j . time ta - i - j corresponds to the time - of - flight for a photon between vehicle 108 and point 706 - j ( i . e ., from transmitter 102 to point 706 - j and back to receiver 104 ), which is the point in zone 704 - j nearest vehicle 108 on detection axis 112 . at sub - operation 903 , reflection 712 - j is detected at spad 502 at detection time tr - j . it should be noted that a reflection is not always detected from each zone 704 . for example , in the example depicted in fig7 - 10 , objects are located only in zones 704 - 2 and 704 - 3 . as a result , no reflection is originated in zone 704 - 1 and vout remains at zero volts throughout sub - gate period 1004 - 1 . at sub - operation 904 , detection time tr - i - j is saved in memory at processor 702 . as discussed above and with respect to system 100 , the use of an nfad in receiver 104 enables detection of multiple reflections within a single detection frame , or in the case of system 700 , within a single sub - gate period . at sub - operation 905 , spad 502 is disarmed at time td - i - j . time td - i - j corresponds to the time - of - flight for a photon between vehicle 108 and point 708 - j , which is the point in zone 704 - j furthest from vehicle 108 on detection axis 112 . in some embodiments , spad 502 is not armed in each sub - gate period within each detection frame . for example , in some embodiments , a spad is armed only during a subset of the sub - gate periods ( e . g ., only during sub - gate period 1004 - 1 ) for a first plurality of detection frames and armed during a different subset of the sub - gate periods ( e . g ., only during sub - gate period 1004 - 2 ) for a second plurality of detection frames , and so on . by dividing each detection frame into a plurality of sub - gate periods , embodiments of the present invention — particularly those embodiments that operate at a wavelength within the range of 1350 nm to 1390 nm — are afforded advantages over prior - art lidar systems that operate at other wavelengths because of a significant reduction in the probability of detecting a photon due to the solar background . for example , prior - art lidar systems operating at a wavelength of 905 nm struggle to overcome the effects of the solar background since their detectors are blinded by solar - based photons on a substantially continuous basis . further , prior - art lidar systems that operate at longer wavelengths , such as 1550 , typically must deal with solar background by restricting fov of each pixel and / or by using very narrow bandwidth filters . for vehicular lidar , however , fov requirements are high . as a result , more restricted - fov pixels must be included to cover the same system - level fov . in addition , it is challenging to provide cost - effective wavelength filters suitable for filtering out solar background , since the filter bandwidth cannot be narrower than the spectrum of the laser used to transmit pulses 110 . embodiments of the present invention avoid the need for restricted fov as well as wavelength filters and , therefore , afford better system performance and lower cost . returning now to method 800 , at operation 802 , digital thresholding is applied to dataset 714 . digital thresholding enables an improvement in the probability of detection ( pd ) of a signal photon while also reducing the impact of “ noise photons ,” such as detected photons arising from events other than reflection from an object ( e . g ., a solar background photon , dark count , and the like ). the negative impact of noise photons on system performance is mitigated by setting a threshold value for the number of reflections detected from a zone during a plurality of detection frames ( e . g ., detections frame - 1 through detection frame - n ), and establishing a position for an object in that zone only when the number of reflections detected is equal to or greater than the threshold value . the positive impact of applying digital thresholding to dataset 714 can be readily seen in table 3 below . careful examination of table 3 shows that , for a solar background of approximately 0 . 5 photons , a threshold value of about 4 signal photons is required at receiver 104 . further , approximately 1 photon due to solar background can be tolerated with 5 signal photons at a threshold level of 8 detection frames where n = 20 . one skilled in the art will recognize that the threshold value is consideration of system design and desired performance and that the threshold value can be any value sufficient to achieve a desired system performance . at operation 803 , processor 106 computes the distance between vehicle 108 and objects located along detection axis 112 . at operation 804 , system 700 rotates detection axis 112 to interrogate a different portion of detection field 114 . at operation 805 , processor 106 develops a map of detection field 114 . it is to be understood that the disclosure teaches just one example of the illustrative embodiment and that many variations of the invention can easily be devised by those skilled in the art after reading this disclosure and that the scope of the present invention is to be determined by the following claims .