US20110188389A1 - Wireless Localisation System - Google Patents
Wireless Localisation System Download PDFInfo
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- US20110188389A1 US20110188389A1 US13/002,640 US200913002640A US2011188389A1 US 20110188389 A1 US20110188389 A1 US 20110188389A1 US 200913002640 A US200913002640 A US 200913002640A US 2011188389 A1 US2011188389 A1 US 2011188389A1
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S5/00—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
- G01S5/02—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using radio waves
- G01S5/14—Determining absolute distances from a plurality of spaced points of known location
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/87—Combinations of radar systems, e.g. primary radar and secondary radar
- G01S13/876—Combination of several spaced transponders or reflectors of known location for determining the position of a receiver
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/87—Combinations of radar systems, e.g. primary radar and secondary radar
- G01S13/878—Combination of several spaced transmitters or receivers of known location for determining the position of a transponder or a reflector
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S5/00—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
- G01S5/01—Determining conditions which influence positioning, e.g. radio environment, state of motion or energy consumption
- G01S5/017—Detecting state or type of motion
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S5/00—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
- G01S5/02—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using radio waves
- G01S5/0205—Details
- G01S5/0218—Multipath in signal reception
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S5/00—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
- G01S5/02—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using radio waves
- G01S5/0205—Details
- G01S5/0226—Transmitters
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S5/00—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
- G01S5/02—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using radio waves
- G01S5/0284—Relative positioning
- G01S5/0289—Relative positioning of multiple transceivers, e.g. in ad hoc networks
Definitions
- the present invention relates generally to wireless localisation, and in particular to tracking objects using radio signals based on measurement of the time-of-arrival.
- a wireless localisation system refers to any system that uses transmission of electromagnetic signals (e.g. radio frequency or microwave) to localise (estimate the location of) an object, in two dimensions or three dimensions.
- Mobile objects can be localised and/or tracked by attaching a signal-enabled tag to the object and using a set of fixed ‘anchor’ nodes in the area to be monitored.
- Inaccuracies in the location estimates arise due to (1) the properties of the radio propagation environment (e.g. multipath reflections and diffraction) and (2) limitations in the system hardware (e.g. lack of time/frequency synchronisation and propagation delays in hardware that are time varying). The latter issues are particularly severe in applications where the anchor nodes have wireless connections and must consist of low-cost hardware.
- RSS received signal strength
- TOA time-of-arrival
- AOA angle-of-arrival
- RSS techniques require expensive hardware to determine the direction of arrival, and may perform poorly in multipath environments where reflections arrive from many directions.
- a common TOA-based technique is satellite navigation (e.g. GPS); however, this is not possible in indoor environments or even in outdoor environments where the accuracy is significantly degraded by multipath signals (e.g. urban canyons).
- the most common TOA-based localisation system uses receiving anchor nodes that are hard-wired (cabled) to the processing hardware (e.g. U.S. Pat. No. 6,831,603). This greatly simplifies the system as a common clock can be shared, eliminating the problem of frequency and time synchronisation. In some situations, such as where rapid installation is required or the region between receiving nodes is inaccessible or inappropriate for cable installation, cabled connections between anchor nodes are impractical.
- the frequency and time synchronisation problem is often handled by using two way (also known as round trip) localisation, and usually also by the use of a reference node (e.g. US Patent 2003/0092448).
- This approach transmits a signal from one node to another, followed immediately by a return signal.
- the time between receiving the forward message and transmitting the reverse message is often assumed to be constant, which is not the case in many practical systems.
- the location of the mobile nodes is estimated in a process known as ‘multilateration’.
- the most common technique uses a minimum mean squared error (MMSE) approach. With this technique, ‘bad’ range data can severely affect the estimated locations of the mobile nodes.
- MMSE minimum mean squared error
- Another technique with a different assumption on the error distribution is based on Projections onto Convex Sets (POCS); however, conventional POCS algorithms do not handle well the case where there is a large intersection region. As with MMSE, the POCS approach is susceptible to bad data due to effects such as multipath reflections, radio interference and fading phenomena.
- a method of computing a round trip delay between a pair of nodes comprising:
- a method of estimating the location of a mobile object using a plurality of ranges between a node associated with said object and respective anchor nodes comprising:
- a method of estimating the location of a mobile object using a plurality of ranges between a node associated with said object and respective anchor nodes comprising:
- each said constraint set being a circle centred on one said anchor node with radius equal to the corresponding range, to obtain an end point;
- said end point is said estimated location of said mobile object.
- a method of time synchronising a plurality of anchor nodes comprising:
- a method of estimating the location of a mobile object using a plurality of anchor nodes comprising:
- a system for estimating the location of one or more objects comprising:
- beacons data capability to send measured times-of-arrival of said beacons, and transmit times of said beacons, to a location server adapted to compute the location of said objects.
- a system for estimating the location of an object comprising:
- a plurality of anchor nodes adapted to communicate wirelessly with each other by either transmitting or receiving beacons;
- a mobile node coincident with said object the mobile node being adapted to communicate wirelessly with said anchor nodes by either transmitting or receiving said beacons;
- a localisation server adapted to:
- the disclosed arrangements include a system for wireless localisation and tracking, and methods that can be used in the disclosed system or other systems.
- the disclosed arrangements estimate object location using multilateration based on measured time-of-arrival (TOA) of radio signals.
- TOA time-of-arrival
- the disclosed arrangements enable more robust processing and hence more accurate location estimation compared to existing systems and methods in the face of bad data due to typical sources of error such as TOA measurement errors (e.g. due to multipath interference or propagation effects), unsynchronised clocks in nodes, time varying propagation delay through the node electronics, and object motion.
- the disclosed system using only low-cost consumer electronic components, is capable of covering large areas (i.e. is not limited to direct radio communication links between all nodes) and is capable of rapid deployment as cabling is not required between any nodes.
- FIG. 1 shows an example of a tracking system within which the disclosed arrangements may be practised
- FIG. 2 is a flow diagram illustrating a general method of localisation according to the preferred embodiment
- FIG. 3 is a schematic block diagram of a general purpose computer upon which disclosed methods can be practised
- FIG. 4 a is an illustration of a beaconing node according to the preferred embodiment
- FIG. 4 b is an illustration of the format of a beacon according to the preferred embodiment
- FIG. 5 is an illustration of an exemplary TDMA beacon schedule
- FIG. 6 is an illustration of a location server according to the preferred embodiment
- FIG. 7 is a flow diagram illustrating a method of estimating the location of mobile nodes according to the preferred embodiment
- FIG. 8 a illustrates a sequence of beacon transmissions
- FIG. 8 b illustrates the motion of a mobile node during the beacon transmissions of FIG. 8 a
- FIG. 9 illustrates the estimation of the location of a node according to the POCS algorithm in an example scenario.
- Appendix A contains pseudocode for a robust MMSE algorithm for estimating the location of a mobile node.
- FIG. 1 shows an example of a tracking system 100 within which the disclosed arrangements may be practised, comprising one soccer player 110 , several fixed anchor nodes, e.g. 120 , surrounding the field, and a location server 130 .
- a tracking system 100 within which the disclosed arrangements may be practised, comprising one soccer player 110 , several fixed anchor nodes, e.g. 120 , surrounding the field, and a location server 130 .
- the anchor nodes 120 are wirelessly connected to the location server to simplify deployment (although where convenient a cable or fibre connection can be used and will usually improve system performance).
- the disclosed tracking system comprises:
- the wireless data communication is preferably performed using direct sequence spread spectrum signalling; however, it could be equally well performed using any radio communication protocol (e.g. the 802.11 family of standards).
- FIG. 2 is a flow diagram illustrating a general method 200 of localisation according to the preferred embodiment.
- step 210 certain nodes called beaconing nodes periodically transmit radio signals called beacons that are received by some other nodes called TOA reception nodes that are able to measure the TOA of the beacon.
- the beacons contain a localisation signal designed for accurate measurement of TOA and an optional data payload. While the localisation signal could be a data symbol, better results are obtained using a specially designed localisation signal.
- the mobile nodes may be beaconing nodes and/or TOA reception nodes, and likewise the anchor nodes may be beaconing nodes and/or TOA reception nodes. For example:
- TDMA time division multiple access
- CDMA code division multiple access
- FDMA frequency division multiple access
- the TOA reception nodes measure the TOA for each received beacon, and at step 230 the TOA reception nodes send the TOA data to the location server (preferably via the data payload in their own beacons, or alternatively via other means such as cable, particularly if a TOA reception node is not also a beaconing node).
- the transmit time of beacons is also required, and beaconing nodes can send this to the location server as a data field in the beacon or by other means. There may be other data such as that related to system operation, for protocols, or from sensors, that is also sent to the location server.
- the location server at step 240 applies a localisation algorithm to the received data to estimate the location of the mobile nodes.
- a beaconing node 400 according to the preferred embodiment is illustrated in FIG. 4 a .
- the beaconing node 400 has digital electronics 430 to generate a beacon and a module 420 to convert the beacon to analog form for radio transmission using a radio transceiver 410 in step 210 of the method 200 .
- the beaconing node 400 also receives data at least to allow synchronisation of TDMA slots, so the data flow in the beaconing node 400 is bidirectional.
- the format of a beacon 450 comprising a header 460 , a data field (payload) 470 , and a TOA localisation signal 480 , is illustrated in FIG. 4 b .
- the TOA localisation signal 480 is specially designed to maximise the accuracy with which the TOA of the signal is measured by a TOA reception node.
- a separate TOA localisation signal 480 is not used and instead a known signal pattern in the header 460 is used to measure the TOA.
- the data field 470 is optional.
- the beacons 450 are scheduled to minimise self-interference and hence maximise localisation accuracy.
- the update rate of a mobile node's location estimate is limited to the rate at which that node transmits beacons.
- Previous schemes for round trip localisation involved a beacon being sent to a node and a reply being immediately generated. For all nodes involved in the measurement (for time synchronisation, propagation delay measurement or mobile node localisation), there is a beacon sent from each node to each of the other nodes. By contrast, according to the disclosed arrangements for round trip localisation, each beaconing node transmits just one beacon per measurement.
- the advantage is that the number of localisation signal transmissions is greatly reduced, which can reduce power consumption and/or increase the number of nodes the system can support. Under the disclosed arrangements, there can be large and variable time intervals between the transmissions of beacons between pairs of nodes. As described in detail below, this time interval is measured and adequately corrected for.
- the preferred TDMA scheme 500 is illustrated in FIG. 5 .
- Time is divided into slots, e.g. 510 , with a beacon being sent in each slot by the node corresponding to the slot label (M 1 is mobile node 1 , A 1 is anchor node 1 , etc).
- a slot can be used by plural nodes, provided the minimum radio link hop count between the nodes using the same slot is greater than two (hence not all nodes have the same schedule).
- the slot size will generally be as small as possible, preferably adjustable between 1 ms and 10 ms.
- the update rate of the beacons is determined by the localisation algorithm category.
- all nodes should transmit at least at the minimum localisation update rate.
- the mobile nodes For mobile transmit localisation, the mobile nodes should transmit at the minimum localisation update rate; however the anchor nodes should transmit at the required rate to maintain time synchronisation, which is in turn dependent upon the stability of the local oscillators in each node.
- the slots are grouped in superframes, e.g. 520 , as this simplifies the TDMA scheme; however, it is not necessary.
- the schedule of each superframe is generally the same, except for dynamic behaviour in the network (e.g. mobile nodes moving in and out of range).
- the scheduling of beacons into slots can be static or dynamic.
- Static allocation in which the schedule is known in advance by all nodes, is simpler but does not allow slot reuse in multi-hop networks.
- Dynamic allocation entails additional communication overhead, either mutually among the nodes according to a distributed algorithm, or between a scheduling controller (e.g. the location server) and the nodes.
- Coarse time synchronisation is required between all nodes for the TDMA scheme; however, this only needs to be within a fraction of the slot duration (e.g. one percent, or 10 ⁇ s for 1 ms slots), which is readily achieved in nodes designed to measure TOA with high accuracy (typically better than 1 ns).
- the synchronisation time reference is provided by one of the nodes either by fixed allocation or selection by the nodes themselves (the latter alternative providing robustness should the time reference node fail). This time synchronisation is too coarse to be of any assistance for localisation.
- TOA reception nodes are adapted to receive a beacon, convert it to digital form, and process it to measure with high resolution the TOA of the beacon (step 220 of the method 200 ).
- a TOA reception node also preferably uses wireless communication to transmit the TOA values to the location server (step 230 of the method 200 ).
- the TOA data is sent to the location server in the data field 470 of the beacon format 450 shown in FIG. 4 b .
- 400 in FIG. 4 a equally well represents a TOA reception node according to the preferred embodiment.
- the measurement of the TOA (step 220 ) is preferably carried out by a TOA reception node according to the method described in the PCT patent application no. PCT/AU2009/000647. However, any technique for the measurement of TOA may alternatively be used.
- a location server 600 according to the preferred embodiment is illustrated in FIG. 6 .
- the location server 600 comprises an analog radio receiver 610 , an analog to digital converter 620 , and digital processing electronics 630 .
- the location server 600 processes the received data from the TOA reception nodes and uses this information to estimate the location of mobile nodes (step 240 ).
- the location server 600 may also perform other functions such as performing and/or reporting system diagnostics and recording and formatting sensor data from the system.
- the digital processing electronics 630 on which the location estimation and any other processing are implemented, are therefore more powerful than the digital processing electronics 430 of either an anchor node or a beacon node.
- the digital processing electronics 630 comprises the digital processing electronics 430 of an anchor node connected via a USB interface to a general purpose computer system 300 such as that shown in FIG. 3 , wherein the processing of step 240 may be implemented as software, such as one or more application programs executable within the computer system 300 .
- the processing of step 240 is effected by instructions in the software that are carried out within the computer system 300 .
- the instructions may be formed as one or more code modules, each for performing one or more particular tasks.
- the software may also be divided into two separate parts, in which a first part and the corresponding code modules performs the location estimation processing and a second part and the corresponding code modules manage an interface between the first part and other systems.
- the software may be stored in a computer readable medium, including the storage devices described below, for example.
- the software is loaded into the computer system 300 from the computer readable medium, and then executed by the computer system 300 .
- a computer readable medium having such software or computer program recorded on it is a computer program product.
- the use of the computer program product in the computer system 300 preferably effects an advantageous apparatus for estimating the location of mobile nodes.
- the computer system 300 is formed by a computer module 301 , input devices such as a keyboard 302 and a mouse pointer device 303 , and output devices including a printer 315 , a display device 314 and loudspeakers 317 .
- An external Modulator-Demodulator (Modem) transceiver device 316 may be used by the computer module 301 for communicating to and from a communications network 320 via a connection 321 .
- the computer module 301 typically includes at least one processor unit 305 , and a memory unit 306 for example formed from semiconductor random access memory (RAM) and read only memory (ROM).
- the module 301 also includes a number of input/output (I/O) interfaces including an audio-video interface 307 that couples to the video display 314 and loudspeakers 317 , an I/O interface 313 for the keyboard 302 and mouse 303 and optionally a joystick (not illustrated), and an interface 308 for the external modem 316 and printer 315 .
- the modem 316 may be incorporated within the computer module 301 , for example within the interface 308 .
- the computer module 301 also has a local network interface 311 which, via a connection 323 , permits coupling of the computer system 300 to a local computer network 322 , known as a Local Area Network (LAN).
- LAN Local Area Network
- the local network 322 may also couple to the wide network 320 via a connection 324 , which would typically include a so-called “firewall” device or similar functionality.
- the interface 311 may be formed by an EthernetTM circuit card, a wireless BluetoothTM or an IEEE 802.11 wireless arrangement.
- the interfaces 308 and 313 may afford both serial and parallel connectivity, the former typically being implemented according to the Universal Serial Bus (USB) standards and having corresponding USB connectors (not illustrated).
- Storage devices 309 are provided and typically include a hard disk drive (HDD) 310 .
- HDD hard disk drive
- Other devices such as a floppy disk drive, a flash memory drive, and a magnetic tape drive (not illustrated) may also be used.
- An optical disk drive 312 is typically provided to act as a non-volatile source of data.
- Portable memory devices, such optical disks (eg: CD-ROM, DVD), USB-RAM, and floppy disks for example may then be used as appropriate sources of data to the system 300 .
- the components 305 , to 313 of the computer module 301 typically communicate via an interconnected bus 304 and in a manner which results in a conventional mode of operation of the computer system 300 known to those in the relevant art.
- Examples of computers on which the described arrangements can be practised include IBM-PC's and compatibles, Sun Sparcstations, Apple MacTM or like computer systems evolved therefrom.
- the application programs discussed above are resident on the hard disk drive 310 and read and controlled in execution by the processor 305 . Intermediate storage of such programs and any data fetched from the networks 320 and 322 may be accomplished using the semiconductor memory 306 , possibly in concert with the hard disk drive 310 . In some instances, the application programs may be supplied to the user encoded on one or more CD-ROM and read via the corresponding drive 312 , or alternatively may be read by the user from the networks 320 or 322 . Still further, the software can also be loaded into the computer system 300 from other computer readable media. Computer readable media refers to any storage medium that participates in providing instructions and/or data to the computer system 300 for execution and/or processing.
- Examples of such media include floppy disks, magnetic tape, CD-ROM, a hard disk drive, a ROM or integrated circuit, a magneto-optical disk, or a computer readable card such as a PCMCIA card and the like, whether or not such devices are internal or external of the computer module 301 .
- Examples of computer readable transmission media that may also participate in the provision of instructions and/or data include radio or infra-red transmission channels as well as a network connection to another computer or networked device, and the Internet or Intranets including e-mail transmissions and information recorded on Websites and the like.
- the second part of the application programs and the corresponding code modules mentioned above may be executed to implement one or more graphical user interfaces (GUIs) to be rendered or otherwise represented upon the display 314 .
- GUIs graphical user interfaces
- a user of the computer system 300 and the application may manipulate the interface to provide controlling commands and/or input to the applications associated with the GUI(s).
- the digital processing electronics 630 may alternatively be dedicated hardware such as one or more integrated circuits performing the functions or sub functions of the step 240 .
- Such dedicated hardware may include graphic processors, digital signal processors, or one or more microprocessors and associated memories with data interfaces (e.g. WLAN or USB or serial interface) but no user interface devices.
- the digital processing electronics 430 of the beaconing/TOA reception node 400 is also preferably dedicated hardware of this kind.
- the location server 600 can utilise round trip or mobile transmit localisation, depending on the specifics of the application.
- An advantage of mobile transmit localisation for tracking objects moving at high velocity is that this approach only uses a single beacon, and is thus only affected by motion for the duration of the beacon (preferably about 0.5 ms).
- the estimation requires all beacons to and from the mobile node in a superframe, which may be extended over a significant period of time (up to 100 ms where 20 slots of 5 ms are used). It is described below how the effect of constant velocity motion can be corrected for under round trip localisation.
- a tradeoff in the choice of the localisation algorithm is that round trip localisation results are degraded by non-constant velocity motion over the superframe, while mobile transmit localisation results are degraded by errors in anchor node time synchronisation.
- the location server 600 can implement multiple localisation algorithms simultaneously, as in the following exemplary scenarios:
- FIG. 7 is a flow diagram illustrating a method 700 according to the preferred embodiment of estimating the location of mobile nodes.
- the main decisions in the method 700 are whether the propagation delay of the anchor nodes is known from prior calibration, and whether mobile transmit or round trip localisation is used.
- round trip localisation with known anchor node propagation delay values there is the further choice of using a MMSE-based or POCS-based localisation algorithm. These choices may be made dynamically, each time the method 700 is executed, or in advance, in which case only the relevant portions of the method 700 need be implemented.
- the steps of the method 700 are mostly carried out by the location server 600 , except for TOA measurement steps 715 , 752 , 735 , 770 , and 775 which are done by beaconing nodes and TOA reception nodes 400 , and the results sent to the location server 600 , as shown by the method 200 .
- the method 700 starts at step 710 where it is determined whether the propagation delay of the anchor nodes is known from prior calibration. If not, the method 700 proceeds to step 715 at which the TOA at each anchor node from all other anchor nodes is measured. In step 720 the corrected round trip delay between each pair of anchor nodes is computed as described below. Step 725 follows, at which the propagation delay at each anchor node is computed as described below.
- step 730 it is checked at step 730 whether round trip localisation is to be used. If not, step 735 measures the TOA at each anchor node from each mobile node.
- Step 740 follows, at which the anchor nodes are time synchronised as described below.
- the Pseudo-Range (see below) between all anchor and mobile nodes is then computed at step 745 as described below, after which at step 750 a robust MMSE-based Time Difference of Arrival (TDOA) algorithm described below is used to estimate the location of each mobile node.
- TDOA Time Difference of Arrival
- step 752 measures the TOA at each anchor node from each mobile node, and vice versa. Then at step 754 , the method 700 computes the Corrected Round Trip Delay between each anchor node and each mobile node as described below. Step 756 follows, at which the Pseudo-Range between all anchor and mobile nodes is computed as described below. Finally at step 758 a robust MMSE-based TOA algorithm, described below, is used to estimate the location of each mobile node.
- step 756 computes range rather than pseudo-range, and step 758 would use either a robust MMSE-based or a POCS-based TOA algorithm, to be described below, to estimate the location of each mobile node from the computed ranges.
- the propagation delay at the mobile nodes is unlikely to be known as the propagation delay of the anchor nodes was initially unknown.
- the method 700 then concludes at step 795 .
- step 765 checks whether round trip localisation is to be used. If not, step 770 measures the TOA at each anchor node from all other anchor nodes and all mobile nodes. The method 700 then continues from step 740 as described above.
- step 775 measures the TOA at each anchor node from each mobile node, and vice versa. Then at step 780 , the method 700 computes the Corrected Round Trip Delay between each anchor node and each mobile node as in step 754 . Step 785 follows, at which the range between all anchor and mobile nodes is computed (assuming the propagation delay at the mobile nodes is known, which is likely since the propagation delay at the anchor nodes is known). Finally at step 790 the robust MMSE- or POCS-based TOA algorithm is used to estimate the location of each mobile node, as in step 758 .
- step 785 computes Pseudo-Range rather than range, and step 790 can only use the robust MMSE-based TOA algorithm, as in step 758 .
- the method 700 then concludes at step 795 .
- the two nodes are labelled as M (typically, but not necessarily, a mobile node) and B (an anchor node).
- Node M transmits a beacon first, followed by node B after a delay of ⁇ MB determined by the beacon schedule (see FIG. 5 ). After a delay of ⁇ SF (the superframe length), this sequence is repeated, as illustrated in FIG. 8 a .
- the beacons are transmitted at times t 1 , t 3 , t 5 and t 7 , and received at times t 2 , t 4 , t 6 and t 8 .
- the difference between the transmit time and the receive time e.g.
- t 2 ⁇ t 1 is the sum of the propagation delay through the transmitter electronics ( ⁇ i tx where i can be M or B), the propagation time through the air (d ij /c where d ij is distance between the two nodes, c is speed of light, and j can be B or M), and the propagation delay through the receiver electronics ( ⁇ j rx ).
- An estimate of the frequency difference between the pair of nodes can be made at node M as follows:
- ⁇ MB is the frequency offset of the local clocks of the node pair
- ⁇ MB is the Doppler frequency shift due to the radial component of the relative motion between the node pair.
- ⁇ MB terms between a mobile node and multiple anchor nodes it is possible to estimate the velocity of the mobile node without determining range or location.
- the round trip delay measurement requires measurements in both directions between the pair of nodes.
- the uncorrected round trip delay, using the first pair of beacons in FIG. 8 a is:
- T MB and D M are directly determined from the measured data, and ⁇ MB is known from the beacon TDMA schedule; if not, it can be readily estimated from the TOA data as follows:
- the location of the mobile node (hence d BM1 ) is unknown, and the propagation delay ⁇ i for each node may be unknown.
- corrected round trip delay measurements are first made between anchor nodes and mobile nodes (steps 754 and 780 ).
- the use of round trip delay measurements for removing the requirement for time synchronisation is well known, but using the corrected round trip delay computed as below, the effects of frequency offset and relative motion can also be removed.
- An important feature of this correction for motion and frequency offset is that it is applied locally to each node pair, and no global processing is required. Note that the motion is corrected to the time at which the mobile node transmits, hence all ranges between this mobile node and multiple anchor nodes are corrected to the same time, compensating for the effect of constant velocity motion.
- the propagation delay ⁇ B of the anchor nodes is either known from prior calibration or computed at step 725 using corrected round trip delay measurements between anchor nodes as described below.
- round trip measurements between mobile nodes are not used, but these measurements may be used for other purposes, e.g. cooperative localisation.
- ⁇ ⁇ is ⁇ ⁇ T MB - ⁇ M - ⁇ B - ⁇ MB ⁇ D M .
- the range between the pair of nodes is therefore computed (step 785 or 756 ) as:
- the location of the mobile node is estimated (step 790 or 758 ).
- ⁇ ⁇ is ⁇ ⁇ T MB - ⁇ B - ⁇ MB ⁇ D M .
- the pseudo-range between the pair of nodes is therefore computed (step 756 or 785 ) as:
- p BM d BM + c ⁇ ⁇ ⁇ M 2 ⁇ c ⁇ T MB - ⁇ B - ⁇ MB ⁇ D M 2 . ( 6 )
- Pre-filtering of the range data improves localisation accuracy by eliminating bad measurements prior to the localisation steps 758 and 790 .
- an improved estimate of the true range at any given time can be determined by a variety of filtering and interpolation operations. Applying these operations prior to estimation of the node location using either the POCS or MMSE approaches described below can result in improved estimation accuracy. Because these operations act on the range data before the localisation step, the result is quite different to applying a filter (such as a Kalman filter or non-linear filter) to the estimated locations.
- a filter such as a Kalman filter or non-linear filter
- any of a number of filtering operations can be applied to the range data, taking into account a priori information about the characteristics of the motion of the mobile node.
- filtering may include for example linear filters (e.g. low pass filter and Kalman filter) or non-linear filters (e.g. median filter).
- linear filters e.g. low pass filter and Kalman filter
- non-linear filters e.g. median filter
- a nonlinear filter which replaces infeasible measurements with a value extrapolated from past measurements can be used.
- One embodiment of such a filter limits the maximum difference in range between the minimum range from of any of the previous 5 superframes and the range from the current superframe.
- the same filtering operations can be applied to pseudo-range data between a given mobile node and anchor nodes, as the distance offset between the pseudo-range and the (unknown) true range is the same for each of these measurements.
- the MMSE cost function to estimate the mobile node location using the range measurements between a mobile node and K anchor nodes is
- w i is an optional weight that is preferably inversely proportional to the noise variance in the range measurement.
- the locations x i of the anchor nodes are known.
- the mobile node location and propagation delay are estimated from the pseudo-range measurements (step 758 or 790 ) as
- Finding the minimising argument of either cost function is a non-linear problem with many solution strategies.
- An initial linear solution followed by one or more non-linear iterations using a Taylor expansion (usually less than five iterations are required) is preferable.
- bad range measurements e.g. ones with a significant bias due to multipath
- An algorithm for doing this is given by the pseudocode in Appendix A.
- the location and the error in the location estimate are computed at line 5 . If the error is less than a threshold, or the number of ranges is less than or equal to a minimum number, the “repeat” loop at line 4 terminates.
- Each range or pseudo-range measurement is then excluded in turn at line 9 , which recomputes the location and the error in the location estimate with the remaining range or pseudo-range measurements.
- the location error estimate is computed as the product of an estimate of the range error and the GDOP (geometric dilution of precision) and is given by:
- Equation (9) is based on the simplifying assumption that the noise in the range (or pseudo-range) measurements is independent and identically distributed, which while not strictly true has been found to work very well with real data.
- the GDOP is calculated as a Cramer-Rao lower bound (see e.g. Larsson, E.G., “Cramer-Rao bound analysis of distributed positioning in sensor networks,” IEEE Signal Processing Letters , vol. 11, no. 3, pp. 334-337, March 2004). This calculation depends upon the location of the anchor nodes, and whether or not the mobile node propagation delay is being estimated.
- the other round-trip localisation approach is the Projection Onto Convex Sets (POCS) algorithm (step 758 or 790 ), where each constraint set is a circle centred on an anchor node with the radius given by the estimated range to that anchor node.
- the POCS algorithm may be extended to 3 dimensional locations by taking the constraint sets as spheres rather than circles.
- the POCS algorithm applies no penalty for the range to the mobile node being less than or equal to the estimated range.
- the POCS algorithm gives good results when large positive errors are likely, such as in indoor environments where the direct path may be severely attenuated by intervening walls.
- a point in the intersection of the constraint sets is found by an iterative process, illustrated in FIG. 9 .
- Constraints sets for three anchor nodes labelled B 1 , B 2 and B 3 are shown as circles centred at each anchor node, with radii equal to the respective ranges from each anchor node.
- a random starting point e.g. 900 or 910 , is updated by projecting onto each of the constraint sets in turn. After a small number of iterations (generally less than 10), the point will be in the (shaded) intersection region 920 of the constraint sets. The end point of the path is recorded.
- the path 915 is taken by the starting point 910 as it is projected onto the constraint sets associated with B 1 , B 2 and B 3 in turn.
- a second path 905 is taken by a starting point 900 as it is projected onto the sets associated with B 3 , B 1 and B 2 in turn.
- the intersection of the constraint sets may be empty. This can be detected by determining whether the end point is not inside all the constraint sets after a substantial number of iterations (preferably 20). There are several possible ways of dealing with this case. In one approach, the ranges to one or more of the anchor nodes are increased by a small amount and the constraint set intersection is recomputed. This is repeated until the intersection of the constraint sets is non-empty. In an alternative approach, a number of different starting points are chosen, and the POCS algorithm is run for a fixed number of iterations for each starting point, and the resulting end points are averaged. In yet another approach, only a single starting point is used, and the solution point is given by the average of the end points over a number of steps of the iterative algorithm.
- intersection of the constraint sets may be empty, it may also be very large, indicated by determining whether multiple end points are widely dispersed. This can be dealt with using strategies similar to those for the case of an empty intersection discussed above.
- the range to at least one of the anchor nodes is decreased and the POCS algorithm run again. This is repeated until the intersection region shrinks to a small size.
- the end point for multiple different starting points may be averaged to estimate the centroid of the constraint set intersection region. In FIG. 9 , the end point for two different starting points is shown. Taking the median of several such end points gives a point near the centroid of the shaded intersection region. The median is the location estimate for the mobile node.
- the location of a mobile node is estimated based on a single beacon from the mobile node to each anchor node. This requires time synchronisation of the anchor nodes (step 740 ) at the time at which the beacon is sent. If the propagation delay of the mobile node is known, it is possible to time synchronise the mobile node to the other nodes and what is generally called a TOA localisation algorithm may be used.
- TDOA Time Difference Of Arrival
- the mobile node is time synchronised, given the transmit time from the mobile t M and a receive time at each anchor node i of t rx,i the measured range between the node pairs is given by
- a set of such measurements can be used as input for the robust MMSE algorithm based on range described above with reference to equation (7). Note that it is not usually convenient to calculate the separate transmit and receive delays, so this localisation algorithm is preferably not used.
- the measured pseudo-range (step 745 ) is
- a set of such measurements can be used as input for the robust MMSE TDOA algorithm based on pseudo-range described above with reference to equation (8), except where above the unknown range offset was c ⁇ M /2, in this case it is c(t M + ⁇ M tx ).
- the propagation delay of anchor nodes at known locations can be readily computed (step 725 ) using the corrected round trip delay
- equation (4) the distance between the anchor nodes i and j is known, as are ⁇ ij and D i using equation (1), so the only unknowns are the propagation delays of the two anchor nodes.
- equation (4) may be rewritten as
- the time offset between anchor nodes is continually changing due to the offset in node clock frequencies (which themselves vary over time). Hence, for the calculation of mobile node location using TDOA, the time offset between the anchor nodes needs to be determined at the time that the mobile node transmitted its beacon (step 740 ). Assume that anchor node i transmits a beacon at t 1 that is received by anchor node j at t 2 . The difference between the measured receive and transmit times at time t 1 is
- t 2 j - t 1 i ⁇ ⁇ j ⁇ ( d ij / c + ⁇ i tx + ⁇ j rx - t 0 , j ) + ⁇ i ⁇ t 0 , i ⁇ ⁇ t 0 , i - t 0 , j + d ij / c + ⁇ i tx + ⁇ j rx .
- d ij is known as the anchor node locations are known, and ⁇ i tx and ⁇ j rx can be solved for, but are actually known from previous calibration or separate anchor node propagation delay calculation (step 725 ).
- the value ⁇ iM can be measured using the receive time of the beacon from the mobile node at node i, however a more robust measurement is to form a least squares estimate of all beacon transmit times over all measurements in a superframe.
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- 2009-07-03 EP EP09771853.0A patent/EP2307902B1/fr active Active
- 2009-07-03 US US13/002,640 patent/US20110188389A1/en not_active Abandoned
- 2009-07-03 WO PCT/AU2009/000863 patent/WO2010000036A1/fr active Application Filing
- 2009-07-03 AU AU2009266425A patent/AU2009266425B2/en active Active
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2016
- 2016-09-01 US US15/255,011 patent/US10338194B2/en active Active
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2019
- 2019-06-27 US US16/454,841 patent/US11061106B2/en active Active
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Also Published As
Publication number | Publication date |
---|---|
US20160370455A1 (en) | 2016-12-22 |
EP2674775B1 (fr) | 2017-01-11 |
EP2674775A1 (fr) | 2013-12-18 |
US11061106B2 (en) | 2021-07-13 |
AU2009266425A1 (en) | 2010-01-07 |
EP2307902A1 (fr) | 2011-04-13 |
EP2307902A4 (fr) | 2011-09-07 |
US20190317184A1 (en) | 2019-10-17 |
EP2307902B1 (fr) | 2013-09-25 |
WO2010000036A1 (fr) | 2010-01-07 |
AU2009266425B2 (en) | 2015-02-05 |
US10338194B2 (en) | 2019-07-02 |
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