Laser radar with reference beam storage

Abstract: In a laser radar system, in which pulses from a laser 1 are focused by a telescope 6 onto a target, the back-scattered radiation being deflected by polarising beam splitter 4 onto a detector 2 in conjunction with a reference beam, the reference beam is produced from pulses derived from the pulse laser 1 by means of the beam splitter 3, the pulses making repeated journeys around a cavity 10 and a proportion of the pulse being emitted each time so that each pulse produces a multiplicity of output pulses to form the reference beam, thereby avoiding the need for a separate laser for the reference beam.

Description: This invention relates to laser radar systems, and especially to pulsed coherent laser radar systems. Pulsed coherent laser radar systems generally use a single frequency laser to generate a sequence of short transmitter pulses. These are focused onto a distant target, and back-scattered light is collected by a receiving telescope mounted close to, or coaxial with, the transmitting optics. The received light is focused onto a photo-detector where it is mixed with a reference beam from a continuous wave laser, tuned to a frequency close to the transmitter frequency. Mixing of the two signals on the detector surface causes a photo-current to be produced at the difference frequency, which current is filtered and rectified. The rectified signal is a sequence of pulses, delayed with respect to transmitter pulses by the round trip transit time to and from the target. The delay time indicates the target range. Coherent systems generally have an advantage in sensitivity over systems using direct detection of the returned light, in which there is no reference beam and thus no interference pattern on the detector. Examples of systems using direct detection of the returned light are rangefinder systems disclosed in DE-A-4 109 844 and EP-A- 0 259 699, in which an optical delay line is used to provide equally spaced reference pulses to evaluate the range from which a transmitted pulse is returned. An example of a coherent system is the radar system disclosed in GB-A-2 111 788, in which a continuous wave laser beam, which is modulated into pulses transmitted for vehicle collision prevention purposes, is split before modulation to provide a continuous beam for the purposes of coherent detection. This invention, however, is concerned with pulsed coherent laser radar systems, in which a laser produces optical pulses for transmission, as opposed to using a continuous wave for transmission, and there is then the need to have a second laser generating a continuous wave reference beam. The power requirement of this laser is modest, a few milliwatts generally being sufficient, but it needs to be maintained at a frequency close to, but not identical to, the transmitter frequency. This is achieved either by continuously tuning one of the lasers with an electro-mechanical eg. piezoelectric actuator to maintain a fixed frequency difference, or by locking the two lasers together, and generating a frequency-offset reference beam with an acousto-optic frequency shifter. Either approach requires an optical system and associated control systems of considerable complexity and high manufacturing cost. The optics are sensitive to thermal drift and mechanical vibration, and so are difficult to construct in a sufficiently rugged form for airborne environments. The invention provides a laser radar system, comprising a laser for producing optical pulses, a detector for receiving radiation back-scattered from an object mixed with a reference laser beam to produce an interference pattern, there being in use a frequency shift between the back-scattered radiation and the reference laser beam so that the detected pulses indicate the range of the object, characterised by an optical delay line, arranged to produce a multiplicity of output pulses, resulting from repeated traversals of the delay line, from each pulse of successive pulses derived from the pulse laser, to form the reference laser beam. The optical delay line provides a quasi-continuous output from a pulsed input and thus produces the reference beam without the need for a separate laser. As well as the cost savings flowing from the omission of the continuous laser, the engineering difficulties of locking lasers together or continuously tuning them to maintain a fixed frequency difference, are avoided. The optical delay line may include reflectors to produce multiple reflections to provide the multiplicity of output pulses. Thus, each pulse of the pulse laser may enter through one reflector, and the output pulse may leave through another reflector which also reflects the pulse around the optical delay line to produce a succession of output pulses. The optical delay line may be a medium such as a fibre or may be free space. In the case where the optical delay line is a length of fibre, a coupler may be provided to produce multiple divisions of each pulse in order to provide the multiplicity of output pulses. A laser radar system constructed in accordance with the invention will now be described, by way of example, with reference to the accompanying drawings in which: Figure 1 is an optical diagram, partly in schematic form, of a laser radar system employing a fibre-optic delay line; Figure 2 illustrates the multiplicity of output pulses produced by a pulse from the pulse laser in figure 1; Figure 3 is an optical diagram, partly in schematic form, of a laser radar system employing another type of fibre-optic delay line; Figure 3a shows the coupling of the fibre-optic ring in enlarged form; Figure 4 is an optical diagram, partly in schematic form, of a laser radar system using a linear delay line; and Figure 5 is an optical diagram, partly in schematic form, of a laser radar system employing a reflective ring delay line. Referring to figure 1, a laser radar system employs a laser for producing optical pulses 1, and a photo-detector 2 for receiving back-scattered radiation mixed with a reference laser beam. The laser is switched to produce a regular sequence of pulses at a single optical frequency. The switching may be by an internal Q-switch or external. Light from the laser 1 passes through a beam splitter 3 which transmits around 90% of the laser pulses to a polarising beam splitter 4 which is orientated with respect to the polarisation of the laser beam to pass the maximum amount of light. Light emerging from the beam splitter 4 passes through a quarter-wave plate 5 which converts it to circularly polarised light. This is the expanded by a telescope 6 which approximately focuses the beam on a distant target (not shown). A small proportion of the light randomly scattered by the target re-enters the telescope 6 and returns along its original path. On passing again through quarter-wave plate 5, it is converted to plane-polarised light with a polarisation orthogonal to that of the transmitted beam. This is diverted by polarising beam splitter 4 and is focused by lens 7 and polariser 8 onto the surface of the photo-detector 2. A reference beam also impinges onto the surface of detector 2, and the wavefront of each beam is coincident as they impinge on the photo-detector 2. The reference frequency is at a fixed frequency difference with respect to the pulses from the laser 1, with the result that an interference pattern is formed on the photo-detector 2 which varies in intensity at the difference frequency. The amplitude of the a.c. photo-current is dependent on the amount of scattering from the target. Each pulse will result in returns from targets at difference ranges over a period of time before the next pulse is transmitted. In accordance with the invention, the reference beam consists of a multiplicity of output pulses from respective pulses derived from the laser 1. Thus, the fraction of each pulse which is reflected by the beam splitter 3 is focused by a lens 9 onto a single mode optical fibre 10 which is provided with reflectors in the form of high reflectance multi-layer dielectric coatings 11 and 12 at each end. The coatings will typically have 98% reflectance and 1.5% transmittance. The fibre 10 has a length such that the time required for light to travel from the input to the far end and back is longer than the length of a laser pulse. Pulses travelling along the fibre are therefore spatially separated from each other. The fibre 10 may be wound on a circular former in such a way that no additional stress is placed on the fibre other than due to bending. Under these circumstances the fibre acts like a birefringent plate so that light entering with polarisation parallel to the ordinary or extraordinary ray directions, emerges from the far end of the fibre with the same polarisation. Light reaching the far end of the fibre is partially transmitted by the high reflectance coating of 11, producing a pulse delayed with respect to the transmitted pulse by the time delay in the fibre, and with the same direction of polarisation as the input pulse. The pulse bounces back and forth between the fibre ends, producing an output pulse at each bounce. The output from the fibre therefore consists of a sequence of pulses of gradually decreasing intensity as shown in figure 2. This sequence of pulses is collimated by a lens 13 and then passes through an acousto-optic frequency shifter 14 which changes the frequency of the light by a small amount. Since the polarisation of the reference beam is the same as that of the main beam pulses, the reference beam is passed by the polarising beam splitter 4. The output of the photo-detector 2 is amplified in amplifier 15 and filtered in filter 16 to remove the low frequency components produced by the reference beam pulse profile. The resulting output 17 consists of a sequence of r.f. pulses at the pulse frequency of the laser, but delayed with respect to the transmitter pulses by the round trip transit time to and from the target. The r.f. frequency will be equal to the frequency shift applied to the reference beam by the frequency shifter 14 plus any Doppler shift due to relative motion between the transmitter/receiver and the target. The reference beam is not a continuous wave, but a sequence of pulses, so that the r.f. signal amplitude emerging from the detector will only be a maximum when the return and reference pulses overlap. This occurs when the round trip transit time to the target is (0.5+m) times the round trip transit time through the fibre 10, where m is zero or an integer. Under these conditions the signal and reference pulses completely overlap, producing maximum output. At other ranges, the r.f. output will be lower because there will only be partial overlap between the return and the reference pulses. There will therefore be a periodic variation in the signal strength with range. This is unlikely to be of much practical importance, however, because the signal strength in coherent detection systems varies randomly over a wide range as a result of laser speckle effects and atmospheric turbulence. In a typical system, the pulses from the laser 1 may be of 0.5 microsecond duration, with a repetition frequency of 500 pulses per second. A typical fibre length for this pulse length would be between 50 and 100 metres to ensure that the pulses do not overlap. Such a fibre could be wound on a circular former typically of 100 to 200 m.m. diameter. The acousto-optic frequency shifter could shift the frequency by a typical amount of 100 MHz, and a Bragg cell could be used for this purpose. While the system described relies on the frequency shifter 14 to produce the frequency shift between the back-scattered radiation and the reference laser beam required for heterodyne detection (an alternating current being produced from the photo-detector 2), the invention is also applicable to homodyne detection. There will usually be a Doppler frequency shift between the laser system and the target, and this can be used to provide the required frequency shift (to provide the a.c. signal). The signal emerging at 17 may be passed to Doppler filter banks or analysed with an FFT (Fast Fourier Transform). The system is applicable for obstacle detection and wind profiling ie. producing a velocity profile of the atmosphere to detect turbulence. Referring to figures 3 and 3a, the laser radar system of figures 1 and 2 may be modified so as to produce the multiplicity of output pulses, not from multiple reflections from the reflectors 11, 12 but rather by using a coupler 18, shown in enlarged form in figure 3a. The other parts of the laser radar system of figure 3 are the same as that of figure 1, and hence will not be described. The coupler 18 is a four-port coupler with weak coupling between, on the one hand, fibre 18a onto one end of which each pulse from the laser 1 is focussed by the lens 9 and from the other end of which radiation is collimated by lens 13 and, on the other hand, a closed ring 18b. The degree of coupling is controlled by the spacing between the fibres in the coupling region. Each pulse from the beam splitter 3 passes directly to collimating lens 13 but a proportion of the power is coupled into the ring 18b. This travels around the ring and a proportion is coupled back into the fibre 18a on each revolution. In this way successive pulses are produced from each pulse derived from the laser 1 via the beam splitter 3. Since the pulse travels once around the loop between each output pulse, to produce the same spacing (figure 2) as for the figure 1 embodiment, it would be necessary for the ring of fibre-optic 18b to be twice the length of the ring 10 of figure 1. Referring to figures 4 and 5 the fibre-optic delay line of figures 1 and 3 may be replaced by a delay line of free space together with reflectors to provide the multiplicity of output pulses from the pulses derived from the pulse laser. In the arrangement of figure 4, a linear delay line is used, and successive output pulses are produced by reflections between reflectors 19, 20. Both reflectors 19, 20 are partially transmitting to allow entry of the input pulse and exit of the output pulses. Reflectors 21 and 22 reflect each pulse derived from the laser 1 via the beam splitter 3 into the cavity and back into the acousto-optic frequency shifter 14. In other respects, the system of figure 4 is the same as that of figures 1 and 3. As another alternative, a reflective delay line 23 may be used (figure 5). Each pulse derived from laser 1 by means of beam splitter 3 is reflected by reflector 22 through reflector 25, which is partially transmitting, and through reflector 24 (also partially transmitting) to be reflected by reflector 21 onto acousto-optic phase shifter 14. At the reflector 24, most of the power of each pulse is reflected to reflector 26 and thence back to reflector 25 and reflector 24, and so on, to produce the multiplicity of output pulses. In this case, pulses partially transmitted by reflector 25 cannot be retro-reflected into the laser, as they can in figure 4, which could be an advantage in certain applications. An advantage of the arrangements of figure 4 and figure 5 compared to those of figures 1 and figure 3 is that an evacuated delay line can be used, thus eliminating attenuation due to materials and permitting operation at wavelengths, such as 10.6 micrometers, which are attenuated in optical materials. It will in fact be easy to arrange that the length traversed between successive output pulses will be less than the pulse length, making the output pulses more quasi-continuous. It will be necessary to set the length with precision in this case, because it will be necessary to ensure that the wavefronts of successive pulses are in phase with each other in the overlap region. Typical laser radars for obstacle avoidance and wind sensing require maximum ranges in the region of 3 to 5 kilometres. The maximum round trip length will therefore be 6 to 10 kilometres. Wavelengths of particular interest are in the eye safe region beyond 1500nm. These include 2.0 to 2.1 micrometres for thulium-YAG and thulium-holmium-YAG lasers and 10.6 micrometres for CO 2 . For 2 micrometres, fluoride fibres could be expected to have low scattering. For low loss materials, the attenuation of the reference pulse amplitude on successive output pulses is dominated by reflectors/coupler losses. Assuming reflectors/couplers with 98% reflectivity/containment, the reference pulse amplitude will be reduced to about 10% of initial amplitude after a time delay equivalent to 3 km range. This should provide sufficient reference beam power to achieve shot-noise limited receiver sensitivity at maximum range. Considering the case of the thulium-YAG laser giving lmJ pulses, 0.5 microseconds long, the peak transmitter power may be approximately 2kW. If 10% of this is diverted to the reference beam, and 5% is admitted into the delay line, the circulating power in the delay line is 3W. Assuming that 1.5% of this is tapped off onto the detector at each exit pulse, and that 70% of this reaches the detector, the reference beam power should be about 30mW initially, reducing to 3mW at 3km range. This should be sufficient to achieve shot-noise limited sensitivity with an optimally designed receiver. The coherent laser radar using a separate laser to provide the reference beam requires both transmitter and reference lasers to operate at a single frequency. If the transmitter laser provides both signal and reference beams, this requirement is no longer necessary, and lasers operating at multiple frequencies can be used. Multi-mode lasers offer considerable practical advantages in terms of output power and efficiency, and in terms of ease of adjustment and low sensitivity to temperature and vibration. Using the delay line, all laser frequencies are present in the reference beam pulses applied to the photo-detector. Components of frequencies are available in the reference beam at all signal frequencies, and so all signal components are coherently detected.

Claims: A laser radar system, comprising a laser (1) for producing optical pulses, a detector (2) for receiving radiation back-scattered from an object mixed with a reference laser beam to produce an interference pattern, there being in use a frequency shift between the back-scattered radiation and the reference laser beam, so that the detected pulses indicate the range of the object, characterised by an optical delay line (10), arranged to produce a multiplicity of output pulses, resulting from repeated traversals of the delay line, from each pulse of successive pulses derived from the pulse laser (1), to form the reference laser beam. A laser radar system as claimed in claim 1, characterised in that the optical delay line (10) includes reflectors (11, 12) to produce multiple reflections from each pulse derived from the pulse laser (1). A laser radar system as claimed in claim 2, characterised in that each pulse is arranged to enter through one reflector (12, 20, 25), a corresponding output pulse leaving through another reflector (11, 19, 24) which also reflects the pulse around the optical delay line (10) to produce the multiplicity of output pulses. A laser radar system as claimed in claim 3, characterised in that there are a pair of reflectors (19, 20) which are parallel to each other. A laser radar system as claimed in claim 3, characterised in that there are more than two reflectors (24, 25, 26) arranged to reflect the pulses around a closed path (23). A laser radar system as claimed in claim 1, characterised in that the optical delay line is a loop (18b) of optical fibre, and a coupler (18) is provided to produce the multiple divisions of each pulse. A laser radar system as claimed in claim 6, characterised in that a four port coupler (18) is provided, two of the ports communicating with the loop of optical fibre (18b), and the other two communicating with an input fibre (18a) for receiving pulses derived from the pulse laser and an output fibre (18a) for carrying the multiplicity of output pulses. A laser radar as claimed in any one of claims 1 to 7, characterised by a frequency shifter (14) for shifting the frequency of the radiation of the reference laser beam.

Inventors: LANGDON ROGER MARTIN DR, LEWIS LLOYD EDWARD, LANGDON, ROGER MARTIN, DR., LEWIS, LLOYD EDWARD
Applicants: MARCONI ELECTRONIC SYST LTD, MARCONI ELECTRONIC SYSTEMS LIMITED
Application year: 1993
Main classification: G01S7
IPC codes: G01S17, G01S7