Location based wireless pet containment system using single base unit

Information

  • Patent Grant
  • 10955521
  • Patent Number
    10,955,521
  • Date Filed
    Monday, December 16, 2019
    5 years ago
  • Date Issued
    Tuesday, March 23, 2021
    3 years ago
Abstract
A wireless animal location system is provided that identifies a location of a pet roaming within an environment using a single base unit. The wireless animal location system tracks and manages animal behavior in the environment using information of pet location.
Description
TECHNICAL FIELD

The disclosure herein involves identifying a location of a roaming object in an environment using wireless communications.


BACKGROUND

Systems and methods have been developed for identifying a location of a roaming object in an environment using wireless communications among multiple base units tracking the object.


INCORPORATION BY REFERENCE

Each patent, patent application, and/or publication mentioned in this specification is herein incorporated by reference in its entirety to the same extent as if each individual patent, patent application, and/or publication was specifically and individually indicated to be incorporated by reference.





BRIEF DESCRIPTION OF THE DRAWINGS


FIG. 1 shows a transceiver of a pet collar communicating with base units, under an embodiment.



FIG. 2 shows a method of trilateration, under an embodiment.



FIG. 3 shows a transceiver of a pet collar communicating with base units, under an embodiment.



FIG. 4 shows a method of trilateration, under an embodiment.



FIG. 5 shows a transceiver of a pet collar communicating with base units, under an embodiment.



FIG. 6A shows a transceiver of a pet collar communicating with a single base unit, under an embodiment.



FIG. 6B shows a top down view of a single base unit, under an embodiment



FIG. 7 shows components of a single base unit, under an embodiment.



FIG. 8 shows an example of range and angular coordinates, under an embodiment.



FIG. 9 shows a function grid superimposed over a monitored area, under an embodiment.



FIG. 10 shows a transceiver of a pet collar communicating with a single base unit, under an embodiment.



FIG. 11 shows a division of space surrounding a single base unit into quadrants, under an embodiment.



FIG. 12 shows a sample computation of an angular value, under an embodiment.



FIG. 13 shows a sample computation of an angular value, under an embodiment.



FIG. 14 shows a sample computation of an angular value, under an embodiment.



FIG. 15 shows a sample computation of an angular value, under an embodiment.





DETAILED DESCRIPTION

A wireless animal location system is provided that identifies a location of a pet roaming within an environment and tracks/manages animal behavior in the environment using information of pet location. The wireless pet location system (or containment system) may disallow access to an area within an environment by applying a negative stimulus when an animal enters a prohibited location. For example, the system may apply a negative stimulus when an animal approaches a pantry space or waste collection space. Conversely, the system may allow the animal free and unimpeded access to other portions of the environment. For example, the system may forgo adverse stimulus when the animal is in desired locations such as animal bedding areas or dedicated animal play areas. The system may simply log an event in order to compile information regarding the animal's behavior. For example, the system may detect and log the presence of the animal near a watering bowl. Further the system may report such information to mobile applications allowing pet owners to monitor and track animal behavior in a home.


An RF-based wireless pet location system may utilize signal strength, two way ranging techniques, and/or time difference of arrival (techniques) to locate a target.


A signal strength based approach uses Received Signal Strength Indicator (RSSI) values to determine the range between a roaming target and three or more spatially separated base units. The target or animal may wear a transceiver housed within a collar. The transceiver may receive and send RF signals to base units. Under an embodiment, three base units within the target's environment periodically transmit RF signals. The pet transceiver estimates its distance from each base unit using the strength of the corresponding RF communication received from each of the base units, i.e. using RSSI values. Based on the multiple ranging measurements, and a known location of the base units within a grid system, a single location may be resolved within the grid system.



FIG. 1 shows an animal worn transceiver 102 in range of three transmitting base units 104, 106, 108. The transceiver 102 communicates with base unit 104, base unit 106, and base unit 108. Based on measured RSSI values, the animal worn collar determines an approximate range from pet to base 104 (−30 dBm, 30 meters), from pet to base 106 (−40 dBm, 40 meters), and from pet to base 108 (−50 dBm, 50 meters). FIG. 2 shows a trilateration method which uses information of the three radii (i.e., distances from transceiver to base units) to identify the location of the pet as a point of intersection between three circles. In other words, base units 104, 106, 108 become center points A, B, C of circles with respective radii of 30 m, 40 m, and 50 m. Since locations of the base units are known within a grid system, the circles intersect at a grid location corresponding to the pet transceiver location. The grid system is established and linked to absolute positions at time of system set-up.


This system requires at least three base units. This complicates the system as an outdoor installation needs to power any unit that is remote to an AC power source. This likely requires that one or more of the base units operate on underground wires or DC power, which is inconvenient if rechargeable, or expensive if primary cells are used. Also, the inclusion of three base units greatly increases the cost of a system. Further, the resultant location is not precise due to the variation of each signal strength determination due to environmental conditions and antenna pattern variation.


A wireless animal location system may use two way ranging (TWR) to determine and monitor animal location under an embodiment. The system may comprise a transceiver housed by a collar worn by an animal and three or more base units distributed in the monitored environment. The system determines the range between the animal target (i.e., animal collar) and the three or more spatially separated base units based on TWR of an RF signal between the target and each of the base units. Based on the multiple time of flight measurements between the collar transceiver and known locations of the base units within a grid system, a single location may be resolved within the grid system.



FIG. 3 shows an animal worn transceiver 302 in range of three transmitting base units 304, 306, 308. The pet transceiver 302 communicates with base unit 304, base unit 306, and base unit 308. During each two way communication, the pet transceiver uses time of flight to determine a range to each base unit. For example. the pet transceiver sends a communication at time t=t0=0. A base unit may process the communication and send a return communication at time t=t1. The pet transceiver (i.e. pet collar) receives the return communication and records the receipt of the communication's first pulse at time t=t2. The time of flight is then computed as (t2−processing time)/2. This time of flight corresponds to a distance. Based on such time of flight calculations, the animal worn collar determines an approximate range from pet to base 304 (30 meters), from pet to base 306 (50 meters), and from pet to base 308 (10 meters). FIG. 4 shows a trilateration method which uses information of the three radii (i.e., distances from transceiver to base units) to identify the location of the pet as a point of intersection between three circles. In other words, base units 304, 306, 308 become center points A, B, C of circles with respective radii of 30 m, 50 m, and 10 m. Since locations of the base units are known within a grid system, the circles intersect at a grid location corresponding to the pet transceiver location.


The system described above requires at least three base units. This complicates the system as an outdoor installation needs to power any unit that is remote to an AC power source. This likely requires that one or more of the base units operate on underground wires or DC power, which is inconvenient if rechargeable, or expensive if primary cells are used. Also, the inclusion of three base units greatly increases the cost of a system.


A wireless animal location system may use time difference of arrival calculations under an embodiment. FIG. 5 shows an animal worn transceiver 502 in range of three transmitting base units 504, 506, 508. The base units 504, 506, 508 communicate 520 with each other to synchronize their respective clocks. The pet collar transceiver 502 periodically transmits RF signals. A pet collar RF transmission is received by base units 504, 506, 508. Upon reception, each base unit time stamps the received signal data. Based on the received times, a location of the pet transceiver may be resolved. Typically, the resolved location is calculated in one of the base units or a remote computer and then communicated to the animal worn transceiver as the animal worn transceiver is typically battery powered and energy conservation is a concern.


The time differential information may be used to determine the difference in distances between the target transceiver 502 and base units 504, 506, 508. The difference in distance information may then be used to determine hyperbolas representing possible locations of the transceiver. The intersection of hyperbolas is then used to locate the pet transceiver in a grid system.



FIG. 6A shows a base unit 602 and an animal worn collar housing a transceiver 604. The base unit comprises antennas 610, 612, 614. FIG. 6B displays a top down view of the base unit. FIGS. 6A & 6B together disclose that the distance between antenna 610 and antenna 614 is d1+d2. The altitude of the triangle (formed by the antennas) extending from antenna 612 is d3. The distance d1 may be equal to distance d2 but embodiments are not so limited. Each antenna may be connected or coupled with a transceiver for sending and receiving RF communications or with a receiver for receiving communications.



FIG. 7 shows a stylized side view of the base unit 702 communicating with a pet transceiver 704 housed by a pet collar. The base unit couples transceiver/antenna 710, receiver/antenna 712, and receiver/antenna 714 with a processing unit 720 which is further connected/coupled to memory 722. The processing unit clocks incoming and/or outgoing communications and synchronizes the transceiver/receivers 710, 712, 714. The base unit emits an RF signal communication 740 using antenna/transceiver 710. The pet transceiver 704 processes the communication and sends a return communication 760. Each antenna unit 710, 712, 714 receives the return communication. The base unit may use two way ranging and the time differential of the return communication received at each transceiver/receiver to resolve a range and angular reference for locating the pet transceiver.



FIG. 8 shows an example of range and angular reference location. FIG. 8 shows an x-y Cartesian coordinate system. The point 810 is located 22 meters from (0,0) and is offset from unit vector (0,1) by 310 degrees (when the angular degree value represents a clockwise rotation of 310 degrees). The range and angular coordinates are then expressed as (22 m, 310 degrees). This coordinate system may be more formally described as a polar coordinate system. A polar coordinate system is a two-dimensional coordinate system in which each point on a plane is determined by a distance from a reference point, i.e. range value, and an angle from a reference direction, i.e. an angular value. The range and angular information may be mapped into Cartesian coordinates as follows:

x=22*cos(140°)=−16.85
y=22*sin(140°)=14.14



FIG. 9 shows a grid superimposed over the monitored area. Each square in the grid corresponds to a set of (range, angular) locations or (x,y) coordinates. Each grid square and corresponding (range, angular) locations may be assigned particular functions. Of course, grid assignments are not restricted to square or rectangular areas. Grid assignments may be assigned to grid portions (i.e. circular, elliptical, manually defined, etc.) and corresponding (range, angular) or (x,y) coordinates.


A grid portion or collection of grid portions may comprise a correction region (i.e. stimulus applied to pet in such region), a keep out region, a containment area, or a notification area. A base unit may transmit appropriate commands to the pet collar when the base unit locates the collar in corresponding grid portions. For example, the base unit may instruct the collar to apply a negative stimulus when the animal is in location 910. The base unit may instruct the collar take no action (or otherwise provide no instruction to take any action) when the animal is at location 914 within containment area 912. The base unit may instruct the collar to apply a negative stimulus when the animal is within a keep out region 916. The base unit may instruct the collar to log the location of the animal when the animal is within location areas 918, 920. Note that a keep out region or a notification region may be assigned to locations within a region that is a general containment area and in which no instruction is generally provided to the animal. This is possible due to the fact that specific areas within the monitored environment may be specifically associated with a function. In this way monitored environment areas 910 and 916 map to a corrective function and monitored environment areas 918, 920 map to logging/notification functions. Under an embodiment, a containment area may simply be all areas in the monitored environment not assigned a correction function.



FIG. 10 shows a top down view of a base unit 1002 communicating with a pet transceiver 1004 housed by a pet collar. The base unit couples transceiver/antenna 1010, receiver/antenna 1012, and receiver/antenna 1014 with a processing unit 1020 which is further connected or coupled to memory (as shown in FIG. 7). The transceiver/antenna 1010, receiver/antenna 1012, and receiver/antenna 1014 may form vertices of an equilateral triangle with sides of 20 cm under one embodiment. The processing unit clocks incoming and/or outgoing communications and synchronizes the transceiver/receivers 1010, 1012, 1014. The base unit emits an RF signal communication (not represented in FIG. 10) using antenna/transceiver 1010. The pet transceiver processes the communication and sends a return communication 1040. Each antenna unit receives the return communication. As further described below, the base unit may use time of flight information received and processed through antenna/transceiver 1010 and time differential of the return communication received at each base unit antenna to resolve a range and angular reference for locating the pet transceiver. A detailed example of this method is provided below.


The transceiver/antenna 1010 transmits an RF message or communication at time 0 seconds. The pet transceiver receives the first pulse of the communication at 66.7128 ns. The pet transceiver then processes the message and develops a response. The pet transceiver transmits the response at 1000 ns. The base unit transceiver/antenna 1010 receives the first pulse of the communication at 1066.7128 ns. The base unit receiver/antenna 1014 receives the first pulse of the communication at 1067.18648 ns. The base unit receiver/antenna 1012 receives the first pulse of the communication at 1067.3572 ns. Note that the data disclosed in this paragraph corresponds to the example set forth below with respect to FIG. 13.


This process collects key information for resolution of a range and angular value for locating the pet transceiver. First, the process reveals the order in which base unit antennas 1010, 1012, 1014 receive the return transmission from the pet transceiver. Second, the process reveals a return time differential between base unit antennas. Continuing with the example set forth above the receive time differential between transceiver/antenna 1010 and receiver/antenna 1014 is 0.47368 ns. Third, the process provides range information. The time of flight between transmission of the response communication and receipt thereof by transceiver/antenna 1010 with respect to the example set forth above comprises 66.7128 ns corresponding to a distance of 20 meters from transceiver/antenna 1010 to pet transceiver. This information may be used to determine range and angular values for locating the pet using a far field model as further described below. Again note that the data disclosed in this paragraph corresponds to the example set forth below with respect to FIG. 13. In addition, the antennas 1010, 1012, 1014 form an equilateral triangles with sides of 20 cm with respect to all of the examples set forth below (see FIGS. 12-14 and corresponding examples).


Under one embodiment, a far field model may determine range and angular values using two way ranging and time difference of arrival computations set forth above. The far field model is based on the fact that the distance from base unit to pet transceiver is significantly farther than the distance between transceiver/receivers of the base unit. This model allows a spherical wave to be approximated by a plane.


The far field model implements the following steps:


Use time of flight information to determine a distance from transceiver/antenna to pet transceiver.


Determine the first two antennas to receive a return transmission from a pet transceiver.


Use the information of the first two receiving antennas to determine an approximate “quadrant” region surrounding the pet (as further shown in FIG. 11 below).


Determine a time difference of arrival between the two first antennas.


Use equations based on an identified region (see FIG. 11 below) to determine angular information. The examples set forth below adopt the base unit configuration of FIG. 10. Further, the examples set forth below assume that the line between antenna 1010 and 1014 represents the reference line for angular values. It is further noted that angular values (in the examples provided below) extend from the reference line in a counter clockwise direction.



FIG. 11 shows an example of quadrant determination based on the time of arrival among antennas. The example shown in FIG. 11 is based on an implementation utilizing a base unit consisting of three transceiver/receivers positioned as an equilateral triangle, although the number and position of transceiver/receivers are not limited to these arrangements. FIG. 11 shows Quadrants I-VI and corresponding order of reception among antennas:


Quadrant I (30-90 degrees): first reception 1014, second reception 1010


Quadrant II (90-150 degrees): first reception 1010, second reception 1014


Quadrant III (150-210 degrees): first reception 1010, second reception 1012


Quadrant IV (210-270 degrees): first reception 1012, second reception 1010


Quadrant V (270-330 degrees): first reception 1012, second reception 1014


Quadrant VI (330-30 degrees): first reception 1014, second reception 1012


As demonstrated by the partitioning of planar space in FIG. 11, order of reception limits the location of the pet transceiver to a particular quadrant or angular region.



FIG. 12 shows a computation of an angular value with respect to a pet location. FIG. 12 show a return RF transmission 1220 from a pet transceiver 1230 located in quadrant I. This is known due to first reception at antenna 1014 and second reception at antenna 1010. Under the far field model, antenna 1010 and 1014 are vertices of a triangle with side 1210 oriented in the general direction of the pet transceiver. The far field model approximates the angle between side 1210 and side 1212 as a ninety (90) degree angle. Again this is possible because the distance between antennas is significantly less than the distance between antennas and pet transceiver. The length L of the line 1214 between antenna 1010 and antenna 1014 is known at 20 cm. FIG. 12 shows the angle θ between lines 1210 and 1214. The length of side 1210 (i.e., the value of D as shown in FIG. 12) may then be computed as follows:


D=CT


C=speed of RF signal from pet transceiver


T=receive time differential between antennas 1010, 1014


Once D is known, there is enough information to solve for θ (as described in greater detail below) and thereby determine an angular value.



FIG. 13 shows an example of a base unit receiving a transmission 1330 from pet transceiver 1320 in Quadrant I. This is known due to first reception at antenna 1014 and second reception at antenna 1010. The time of flight and corresponding distance between antenna 1010 and pet transceiver 1320 is 66.7128 ns and 20 m. Antenna 1010 and 1014 form vertices of a triangle with side 1310 oriented in the general direction of the pet transceiver. The angle between sides 1310 and 1312 is approximated as 90 degrees under the far field model. The length of side 1314 is known at 20 cm. The time differential between antennas 1010 and 1014 is 0.47368 ns. The length D of side 1310 may now be computed. Further, the value of θ may be calculated by first computing the value of α as follows:






α
=



sin

-
1




(


C

T

L

)


=



sin

-
1


[



(


30





cm

ns

)

*

(


.
4


7368





ns

)



20





cm


]

=


sin

-
1




[
.71052
]










α
=


4


5
.
2


7


8







θ

=



1

8


0



-

9


0



-

4


5
.
2


7


8




=

4


4
.
7


2


3










Therefore the location of the pet may be approximated with a range, angular value of (20 m, 44.723).



FIG. 14 shows an example of a base unit receiving a transmission 1430 from pet transceiver 1420 in Quadrant II. This is known due to first reception at antenna 1010 and second reception at antenna 1014. It is assumed the time of flight between pet transceiver 1420 and antenna 1010 indicates a distance of 20 m. Antenna 1010 and 1014 form vertices of a triangle with side 1410 oriented in the general direction of the pet transceiver. The angle between sides 1410 and 1412 is approximated as 90 degrees under the far field model. The length of side 1414 is known at 20 cm. The time differential between antennas 1010 and 1014 is 0.56245 ns. The length D of side 1410 may now be computed. The value of θ may be calculated by first computing the value of α as follows:






α
=



cos

-
1




(


C

T

L

)


=



cos

-
1


[



(


30





cm

ns

)

*

(


.
5


6245





ns

)



20





cm


]

=

3


2
.
4



7











α
=

3


2
.
4



7









θ
=



1

8


0



-
α

=



1

8


0



-

3


2
.
4



7




=

1

4


7
.
5



3










Therefore the location of the pet may be approximated with a range, angular value of (20 m, 147.53).



FIG. 15 shows an example of a base unit receiving a transmission 1530 from pet transceiver 1520 in Quadrant III. This is known due to first reception at antenna 1012 and second reception at antenna 1010. It is assumed the time of flight between pet transceiver 1520 and antenna 1012 indicates a distance of 20 m. Antenna 1010 and 1012 form vertices of a triangle with side 1510 oriented in the general direction of the pet transceiver. The angle between sides 1510 and 1512 is approximated as 90 degrees under the far field model. The length of side 1514 is known at 20 cm. The time differential between antennas 1010 and 1012 is 0.5342 ns. The length D of side 1510 may now be computed. Further, the value of θ may be calculated by first computing the value of Ø and α as follows:







=



sin

-
1




(


C

T

L

)


=



sin

-
1




[



(


30





cm

ns

)

*

(


.
5


342





ns

)



20





cm


]


=



sin

-
1




[
.8013
]


=

5


3
.
2



5

















α
=



18


0



-

9


0



-

5


3
.
2



5




=

3


6
.
7



5
















θ
=



18


0



-

3


6
.
7



5




=

1

4


3
.
2



5










Therefore the location of the pet may be approximated with a range, angular value of (20 m, 263.25). In this case, it is known based on time differential that the pet transceiver is located in Quadrant III. This means that θ is computed with respect to antennas 1010 and 1012. Therefore, the angular value must be approximated by adding 120° such that the angular value sweeps through Quadrant I and Quadrant II and then an additional 143.25° through Quadrant III. In like manner, angular estimates for the pet transceiver in quadrants IV, V, and VI should add 180°, 240°, and 300° respectively.


It should be further noted that angle computations are applied according the detected position of the pet transceiver. As indicated above, it is known based on receive time differentials that the pet transceiver is located in one of Quadrants I-VI. As one example, the pet transceiver may be located in Quadrant V. Therefore, a known computation may be applied to determine an angular location of the animal with respect to a line between antennas 1012 and 1014. Assuming the facts set forth above with respect to FIGS. 12-16, an additional 240 degrees is then added to the angular estimate. The pet transceiver is then located at the adjusted angular estimate (with respect to the line between antennas 1010 and 1014, i.e. the zero angular reference) and approximately 20 meters from the base unit.


The examples presented above utilize three antennas in an equilateral triangle configuration, however this is not a limitation as the number of antennas can be any number greater than three, or greater than two if a physical limitation exists to block 180 degrees of the coverage of the area. Further, the configuration of antennas is not limited to any specific trigonometric configuration.


It should be noted that the time difference of arrival among transceiver/antennas and/or receiver/antennas may be determined by the difference in phase of the carrier signal of an incoming signal.


Three dimensional positional resolution can also be performed. It can be treated as two separate two-dimensional position resolutions in two perpendicular planes as long as there are positional differences between the antennas in the two planes.


A device is described that comprises under an embodiment a base unit including a first transceiver, a second receiver, and a third receiver, wherein the first transceiver comprises a first antenna, the second receiver comprises a second antenna, and the third receiver comprises a third antenna, wherein the first transceiver, the second receiver, and the third receiver are communicatively coupled with at least one processor of the base unit, wherein the base unit comprises a clock that synchronizes communications of the first transceiver, the second receiver, and the third receiver, wherein the first transceiver, the second receiver, and the third receiver comprise vertices of a triangle. The base unit includes the first transceiver configured to transmit a communication to a transceiver remote to the base unit. The base unit includes the first transceiver, the second receiver, and the third receiver configured to receive a response from the transceiver, wherein the response comprises a return communication. The base unit includes the at least one processor configured to use information of the return communication to determine a first time of flight, wherein the first time of flight comprises the time elapsed between transmission of the return communication and the receiving of the return communication by the first transceiver. The base unit includes the at least one processor configured to use the first time of flight to determine a first distance between the first transceiver and the transceiver. The base unit includes the at least one processor configured to use the clock to determine a time difference of arrival between the first transceiver receiving the return communication, the second receiver receiving the return communication, and the third receiver receiving the return communication. The base unit includes the at least one processor configured to determine an angular value using information of the time difference of arrival, the relative positioning of the first antenna, the second antenna, and the third antenna and signal transmission speed of the return communication, wherein the angular value comprises an angle between a reference direction and an axis, wherein the angular value and the first distance approximate a location of the transceiver.


The triangle of an embodiment comprises an equilateral triangle.


Sides of the equilateral triangle are equal to or less than 20 cm, under an embodiment.


The at least one processor of an embodiment is configured to determine the time difference of arrival using the difference in phase of a carrier signal of the return communication among the first transceiver, the second receiver, and the third receiver.


The reference direction of an embodiment comprises a fixed unit vector originating at a vertex of the triangle and extending along a side of the triangle.


The vertices of the triangle approximately define a plane, wherein a plurality of quadrants partition the plane into radial segments extending from the base unit, under an embodiment.


The information of the time difference of arrival comprises an order of reception between the initial two antennas receiving the return communication, under an embodiment.


The determining the angular value includes using the order of reception between the initial two antennas to locate the transceiver in a quadrant of the plurality of quadrants, under an embodiment.


The determining the angular value includes under an embodiment constructing a right triangle, wherein the initial two antennas comprise vertices of the right triangle, wherein a first side of the right triangle is oriented in a direction of the transceiver in the quadrant, wherein a second side comprises a line between the initial two antennas.


The determining the angular value includes under an embodiment determining a first length of the first side using the signal transmission speed and the time difference of arrival between the initial two antennas receiving the return communication.


A second length comprises a length of the second side, under an embodiment.


The determining the angular value comprises under an embodiment determining the angular value using the first length, the second length, and information of the quadrant.


The transceiver of an embodiment is communicatively coupled with a stimulus unit positioned in a collar worn by an animal.


The at least one processor of an embodiment is configured to identify at least one instruction using the first distance and the angular value.


The at least one instruction of an embodiment includes logging the first distance and the angular value.


The identifying the at least one instruction includes transmitting the at least one instruction to the transceiver, under an embodiment.


The at least one instruction includes an instruction to apply a positive stimulus, under an embodiment.


The at least one instruction includes an instruction to apply a negative stimulus, under an embodiment.


A device is described that comprises under an embodiment a base unit including at least three transceivers, wherein the at least three transceivers are communicatively coupled with at least one processor of the base unit, wherein the base unit comprises a clock that synchronizes communications of the at least three transceivers. The device includes a first transceiver of the at least three transceivers configured to transmit a communication to a transceiver remote to the base unit. The device includes the at least three transceivers configured to receive a response from the transceiver, wherein the response comprises a return communication. The device includes the at least one processor configured to use information of the return communication to determine a first time of flight, wherein the first time of flight comprises the time elapsed between transmission of the return communication and the receiving of the return communication by the first transceiver. The device includes the at least one processor configured to use the first time of flight to determine a first distance between the first transceiver and the transceiver. The device includes the at least one processor configured to use the clock to determine a time difference of arrival among the at least three transceivers receiving the return communication. The device includes the at least one processor configured to determine an angular value using information of the time difference of arrival, the relative positioning of the at least three transceivers and signal transmission speed of the return communication, wherein the angular value comprises an angle between a reference direction and an axis, wherein the angular value and the first distance approximate a location of the transceiver.


Computer networks suitable for use with the embodiments described herein include local area networks (LAN), wide area networks (WAN), Internet, or other connection services and network variations such as the world wide web, the public internet, a private internet, a private computer network, a public network, a mobile network, a cellular network, a value-added network, and the like. Computing devices coupled or connected to the network may be any microprocessor controlled device that permits access to the network, including terminal devices, such as personal computers, workstations, servers, mini computers, main-frame computers, laptop computers, mobile computers, palm top computers, hand held computers, mobile phones, TV set-top boxes, or combinations thereof. The computer network may include one of more LANs, WANs, Internets, and computers. The computers may serve as servers, clients, or a combination thereof.


The wireless pet containment system using a single base unit can be a component of a single system, multiple systems, and/or geographically separate systems. The wireless pet containment system using a single base unit can also be a subcomponent or subsystem of a single system, multiple systems, and/or geographically separate systems. The components of wireless pet containment system using a single base unit can be coupled to one or more other components (not shown) of a host system or a system coupled to the host system.


One or more components of the wireless pet containment system using a single base unit and/or a corresponding interface, system or application to which the wireless pet containment system using a single base unit is coupled or connected includes and/or runs under and/or in association with a processing system. The processing system includes any collection of processor-based devices or computing devices operating together, or components of processing systems or devices, as is known in the art. For example, the processing system can include one or more of a portable computer, portable communication device operating in a communication network, and/or a network server. The portable computer can be any of a number and/or combination of devices selected from among personal computers, personal digital assistants, portable computing devices, and portable communication devices, but is not so limited. The processing system can include components within a larger computer system.


The processing system of an embodiment includes at least one processor and at least one memory device or subsystem. The processing system can also include or be coupled to at least one database. The term “processor” as generally used herein refers to any logic processing unit, such as one or more central processing units (CPUs), digital signal processors (DSPs), application-specific integrated circuits (ASIC), etc. The processor and memory can be monolithically integrated onto a single chip, distributed among a number of chips or components, and/or provided by some combination of algorithms. The methods described herein can be implemented in one or more of software algorithm(s), programs, firmware, hardware, components, circuitry, in any combination.


The components of any system that include the wireless pet containment system using a single base unit can be located together or in separate locations. Communication paths couple the components and include any medium for communicating or transferring files among the components. The communication paths include wireless connections, wired connections, and hybrid wireless/wired connections. The communication paths also include couplings or connections to networks including local area networks (LANs), metropolitan area networks (MANs), wide area networks (WANs), proprietary networks, interoffice or backend networks, and the Internet. Furthermore, the communication paths include removable fixed mediums like floppy disks, hard disk drives, and CD-ROM disks, as well as flash RAM, Universal Serial Bus (USB) connections, RS-232 connections, telephone lines, buses, and electronic mail messages.


Aspects of the wireless pet containment system using a single base unit and corresponding systems and methods described herein may be implemented as functionality programmed into any of a variety of circuitry, including programmable logic devices (PLDs), such as field programmable gate arrays (FPGAs), programmable array logic (PAL) devices, electrically programmable logic and memory devices and standard cell-based devices, as well as application specific integrated circuits (ASICs). Some other possibilities for implementing aspects of the wireless pet containment system using a single base unit and corresponding systems and methods include: microcontrollers with memory (such as electronically erasable programmable read only memory (EEPROM)), embedded microprocessors, firmware, software, etc. Furthermore, aspects of the wireless pet containment system using a single base unit and corresponding systems and methods may be embodied in microprocessors having software-based circuit emulation, discrete logic (sequential and combinatorial), custom devices, fuzzy (neural) logic, quantum devices, and hybrids of any of the above device types. Of course the underlying device technologies may be provided in a variety of component types, e.g., metal-oxide semiconductor field-effect transistor (MOSFET) technologies like complementary metal-oxide semiconductor (CMOS), bipolar technologies like emitter-coupled logic (ECL), polymer technologies (e.g., silicon-conjugated polymer and metal-conjugated polymer-metal structures), mixed analog and digital, etc.


It should be noted that any system, method, and/or other components disclosed herein may be described using computer aided design tools and expressed (or represented), as data and/or instructions embodied in various computer-readable media, in terms of their behavioral, register transfer, logic component, transistor, layout geometries, and/or other characteristics. Computer-readable media in which such formatted data and/or instructions may be embodied include, but are not limited to, non-volatile storage media in various forms (e.g., optical, magnetic or semiconductor storage media) and carrier waves that may be used to transfer such formatted data and/or instructions through wireless, optical, or wired signaling media or any combination thereof. Examples of transfers of such formatted data and/or instructions by carrier waves include, but are not limited to, transfers (uploads, downloads, e-mail, etc.) over the Internet and/or other computer networks via one or more data transfer protocols (e.g., HTTP, FTP, SMTP, etc.). When received within a computer system via one or more computer-readable media, such data and/or instruction-based expressions of the above described components may be processed by a processing entity (e.g., one or more processors) within the computer system in conjunction with execution of one or more other computer programs.


Unless the context clearly requires otherwise, throughout the description and the claims, the words “comprise,” “comprising,” and the like are to be construed in an inclusive sense as opposed to an exclusive or exhaustive sense; that is to say, in a sense of “including, but not limited to.” Words using the singular or plural number also include the plural or singular number respectively. Additionally, the words “herein,” “hereunder,” “above,” “below,” and words of similar import, when used in this application, refer to this application as a whole and not to any particular portions of this application. When the word “or” is used in reference to a list of two or more items, that word covers all of the following interpretations of the word: any of the items in the list, all of the items in the list and any combination of the items in the list.


The above description of embodiments of the wireless pet containment system using a single base unit is not intended to be exhaustive or to limit the systems and methods to the precise forms disclosed. While specific embodiments of, and examples for, the wireless pet containment system using a single base unit and corresponding systems and methods are described herein for illustrative purposes, various equivalent modifications are possible within the scope of the systems and methods, as those skilled in the relevant art will recognize. The teachings of the wireless pet containment system using a single base unit and corresponding systems and methods provided herein can be applied to other systems and methods, not only for the systems and methods described above.


The elements and acts of the various embodiments described above can be combined to provide further embodiments. These and other changes can be made to the wireless pet containment system using a single base unit and corresponding systems and methods in light of the above detailed description.

Claims
  • 1. A method comprising, a clock synchronizing communications of at least three transceivers, wherein each transceiver of the at least three transceivers includes an antenna, wherein the at least three transceivers occupy a plane;a first transceiver of the at least three transceivers transmitting a communication to a remote transceiver;the at least three transceivers receiving a response to the communication from the remote transceiver, wherein the response comprises a return communication;using information of the return communication to determine a first time of flight, wherein the first time of flight comprises the time elapsed between transmission of the return communication and the receiving of the return communication by the first transceiver;using the first time of flight to determine a first distance between the first transceiver and the remote transceiver;using the clock to determine a time difference of arrival of the return communication between the first transceiver of the at least three transceivers and the remaining receivers of the at least three transceivers;determining an angular value using information of the time difference of arrival, the relative positioning of the at least three transceivers, and signal transmission speed of the return communication, wherein the angular value comprises an angle between a reference direction and an axis, wherein the reference direction comprises a fixed unit vector originating at a location of a transceiver of the at least three transceivers, wherein the information of the time difference of arrival includes an order of reception between an initial two transceivers of the at least three transceivers receiving the return communication, wherein the angular value and the first distance approximate a location of the transceiver.
  • 2. The method of claim 1, wherein the at least three transceivers include three transceivers comprising vertices of an equilateral triangle.
  • 3. The method of claim 2, wherein sides of the equilateral triangle are equal to or less than 20 cm.
  • 4. The method of claim 2, wherein the reference direction comprises a fixed unit vector originating at a vertex of the triangle and extending along a side of the triangle.
  • 5. The method of claim 4, wherein a plurality of quadrants partition the plane into radial segments extending from the base unit.
  • 6. The method of claim 5, comprising using the order of reception to estimate a first location of the remote transceiver in the plane.
  • 7. The method of claim 6, wherein the estimated first location comprises a location of the remote transceiver in a quadrant of the plurality of quadrants.
  • 8. The method of claim 7, the determining the angular value including constructing a right triangle, wherein the initial two antennas comprise vertices of the right triangle, wherein a first side of the right triangle is oriented in a direction of the remote transceiver in the quadrant, wherein a second side comprises a line between the initial two antennas.
  • 9. The method of claim 8, the determining the angular value including determining a first length of the first side using the signal transmission speed and the time difference of arrival between the initial two antennas receiving the return communication.
  • 10. The method of claim 9, wherein a second length comprises a length of the second side.
  • 11. The method of claim 10, the determining the angular value comprising determining the angular value using the first length, the second length, and information of the quadrant.
  • 12. The method of claim 1, wherein the remote transceiver is communicatively coupled with a stimulus unit positioned in a collar worn by an animal.
  • 13. The method of claim 12, comprising identifying at least one instruction using the first distance and the angular value.
  • 14. The method of claim 13, the at least one instruction including logging the first distance and the angular value.
  • 15. The method of claim 14, the identifying the at least one instruction including transmitting the at least one instruction to the remote transceiver.
  • 16. The method of claim 15, the at least one instruction including an instruction to apply a positive stimulus.
  • 17. The method of claim 16, the at least one instruction including an instruction to apply a negative stimulus.
  • 18. The method of claim 1, the determining the time difference of arrival comprising using a difference in phase of a carrier signal of the return communication among the at least three transceivers to determine the time difference of arrival.
  • 19. A method comprising, a clock synchronizing communications of a first transceiver, a second receiver, and a third receiver, wherein the first transceiver comprises a first antenna, the second receiver comprises a second antenna, and the third receiver comprises a third antenna, wherein the first transceiver, the second receiver, and the third receiver occupy a plane;the first transceiver transmitting a communication to a remote transceiver;the first transceiver, the second receiver, and the third receiver receiving a response from the remote transceiver, wherein the response comprises a return communication;using information of the return communication to determine a first time of flight, wherein the first time of flight comprises the time elapsed between transmission of the return communication and the receiving of the return communication by the first transceiver;using the first time of flight to determine a first distance between the first transceiver and the remote transceiver;using the clock to determine a time difference of arrival between the first transceiver receiving the return communication, the second receiver receiving the return communication, and the third receiver receiving the return communication;using information of the time difference of arrival to determine an order of reception between an initial two antennas of the first antenna, the second antenna, and the third antenna receiving the return communication;using the order of reception to estimate a first location of the remote transceiver in the plane;determining an angular value using information of the time difference of arrival, the relative positioning of the first antenna, the second antenna, and the third antenna, signal transmission speed of the return communication, and the estimated first location, wherein the angular value comprises an angle between a reference direction and an axis, wherein the reference direction comprises a fixed unit vector originating at a location of at least one of the first antenna, the second antenna, and the third antenna, wherein the angular value and the first distance approximate a location of the remote transceiver.
RELATED APPLICATIONS

This application is a continuation application of U.S. application Ser. No. 16/003,876, filed Jun. 8, 2018, which claims the benefit of U.S. Application No. 62/599,248, filed Dec. 15, 2017.

US Referenced Citations (389)
Number Name Date Kind
2364994 Moore Dec 1944 A
2741224 Putnam Apr 1956 A
3182211 Maratuech May 1965 A
3184730 Irish May 1965 A
3500373 Arthur Mar 1970 A
3735757 MacFarland May 1973 A
4180013 Smith Dec 1979 A
4426884 Polchaninoff Jan 1984 A
4783646 Matsuzaki Nov 1988 A
4794402 Gonda et al. Dec 1988 A
4802482 Gonda et al. Feb 1989 A
4947795 Farkas Aug 1990 A
4969418 Jones Nov 1990 A
5054428 Farkus Oct 1991 A
5159580 Andersen et al. Oct 1992 A
5161485 McDade Nov 1992 A
5182032 Dickie et al. Jan 1993 A
5207178 McDade et al. May 1993 A
5207179 Arthur et al. May 1993 A
5526006 Akahane et al. Jun 1996 A
5559498 Westrick et al. Sep 1996 A
5576972 Harrison Nov 1996 A
5586521 Kelley Dec 1996 A
5601054 So Feb 1997 A
5642690 Calabrese et al. Jul 1997 A
5794569 Titus et al. Aug 1998 A
5815077 Christiansen Sep 1998 A
5844489 Yarnall, Jr. et al. Dec 1998 A
5857433 Files Jan 1999 A
5870029 Otto et al. Feb 1999 A
5872516 Bonge, Jr. Feb 1999 A
5886669 Kita Mar 1999 A
5913284 Van Curen et al. Jun 1999 A
5923254 Brune Jul 1999 A
5927233 Mainini et al. Jul 1999 A
5933079 Frink Aug 1999 A
5934225 Williams Aug 1999 A
5949350 Girard et al. Sep 1999 A
5957983 Tominaga Sep 1999 A
5982291 Williams et al. Nov 1999 A
6016100 Boyd et al. Jan 2000 A
6019066 Taylor Feb 2000 A
6028531 Wanderlich Feb 2000 A
6047664 Lyerly Apr 2000 A
6067018 Skelton et al. May 2000 A
6075443 Schepps et al. Jun 2000 A
6166643 Janning et al. Dec 2000 A
6170439 Duncan et al. Jan 2001 B1
6184790 Gerig Feb 2001 B1
6196990 Zicherman Mar 2001 B1
6204762 Dering et al. Mar 2001 B1
6215314 Frankewich, Jr. Apr 2001 B1
6230031 Barber May 2001 B1
6230661 Yarnall, Jr. et al. May 2001 B1
6232880 Anderson et al. May 2001 B1
6271757 Touchton et al. Aug 2001 B1
6327999 Gerig Dec 2001 B1
6353390 Beri et al. Mar 2002 B1
6360697 Williams Mar 2002 B1
6360698 Stapelfeld et al. Mar 2002 B1
6404338 Koslar Jun 2002 B1
6415742 Lee et al. Jul 2002 B1
6426464 Spellman et al. Jul 2002 B1
6427079 Schneider et al. Jul 2002 B1
6431121 Mainini et al. Aug 2002 B1
6431122 Westrick et al. Aug 2002 B1
6441778 Durst et al. Aug 2002 B1
6459378 Gerig Oct 2002 B2
6487992 Hollis Dec 2002 B1
6561137 Oakman May 2003 B2
6581546 Dalland et al. Jun 2003 B1
6588376 Groh Jul 2003 B1
6598563 Kim et al. Jul 2003 B2
6600422 Barry et al. Jul 2003 B2
6637376 Lee et al. Oct 2003 B2
6657544 Barry et al. Dec 2003 B2
6668760 Groh et al. Dec 2003 B2
6700492 Touchton et al. Mar 2004 B2
6747555 Fellenstein et al. Jun 2004 B2
6798887 Andre Sep 2004 B1
6799537 Liao Oct 2004 B1
6807720 Brune et al. Oct 2004 B2
6820025 Bachmann et al. Nov 2004 B2
6825768 Stapelfeld et al. Nov 2004 B2
6830012 Swan Dec 2004 B1
6833790 Mejia et al. Dec 2004 B2
6874447 Kobett Apr 2005 B1
6888502 Beigel et al. May 2005 B2
6901883 Gillis et al. Jun 2005 B2
6903682 Maddox Jun 2005 B1
6907844 Crist et al. Jun 2005 B1
6907883 Lin Jun 2005 B2
6921089 Groh et al. Jul 2005 B2
6923146 Korbitz et al. Aug 2005 B2
6928958 Crist et al. Aug 2005 B2
6937647 Boyd et al. Aug 2005 B1
6956483 Schmitt et al. Oct 2005 B2
6970090 Sciarra Nov 2005 B1
7061385 Fong et al. Jun 2006 B2
7079024 Alarcon et al. Jul 2006 B2
7114466 Mayer Oct 2006 B1
7142167 Rochelle et al. Nov 2006 B2
7164354 Panzer Jan 2007 B1
7173535 Bach et al. Feb 2007 B2
7198009 Crist et al. Apr 2007 B2
7222589 Lee et al. May 2007 B2
7249572 Goetzl et al. Jul 2007 B2
7252051 Napolez et al. Aug 2007 B2
7259718 Patterson et al. Aug 2007 B2
7267081 Steinbacher Sep 2007 B2
7275502 Boyd et al. Oct 2007 B2
7296540 Boyd Nov 2007 B2
7319397 Chung et al. Jan 2008 B2
7328671 Kates Feb 2008 B2
7339474 Easley et al. Mar 2008 B2
7382328 Lee, IV et al. Jun 2008 B2
7394390 Gerig Jul 2008 B2
7395966 Braiman Jul 2008 B2
7404379 Nottingham et al. Jul 2008 B2
7411492 Greenberg et al. Aug 2008 B2
7426906 Nottingham et al. Sep 2008 B2
7434541 Kates Oct 2008 B2
7443298 Cole et al. Oct 2008 B2
7477155 Bach et al. Jan 2009 B2
7503285 Mainini et al. Mar 2009 B2
7518275 Suzuki et al. Apr 2009 B2
7518522 So et al. Apr 2009 B2
7538679 Shanks May 2009 B2
7546817 Moore Jun 2009 B2
7552699 Moore Jun 2009 B2
7559291 Reinhart Jul 2009 B2
7562640 Lalor Jul 2009 B2
7565885 Moore Jul 2009 B2
7574979 Nottingham et al. Aug 2009 B2
7583931 Eu et al. Sep 2009 B2
7602302 Hokuf et al. Oct 2009 B2
7612668 Harvey Nov 2009 B2
7616124 Paessel et al. Nov 2009 B2
7656291 Rochelle et al. Feb 2010 B2
7658166 Rheinschmidt, Jr. et al. Feb 2010 B1
7667599 Mainini et al. Feb 2010 B2
7667607 Gerig et al. Feb 2010 B2
7680645 Li et al. Mar 2010 B2
7705736 Kedziora Apr 2010 B1
7710263 Boyd May 2010 B2
7760137 Martucci et al. Jul 2010 B2
7779788 Moore Aug 2010 B2
7786876 Troxler et al. Aug 2010 B2
7804724 Way Sep 2010 B2
7814865 Tracy et al. Oct 2010 B2
7828221 Kwon, II Nov 2010 B2
7830257 Hassell Nov 2010 B2
7834769 Hinkle et al. Nov 2010 B2
7841301 Mainini et al. Nov 2010 B2
7856947 Giunta Dec 2010 B2
7864057 Milnes et al. Jan 2011 B2
7868912 Venetianer et al. Jan 2011 B2
7900585 Lee et al. Mar 2011 B2
7918190 Belcher et al. Apr 2011 B2
7944359 Fong et al. May 2011 B2
7946252 Lee, IV et al. May 2011 B2
7978078 Copeland et al. Jul 2011 B2
7996983 Lee et al. Aug 2011 B2
8011327 Mainini et al. Sep 2011 B2
8047161 Moore et al. Nov 2011 B2
8049630 Chao et al. Nov 2011 B2
8065978 Duncan et al. Nov 2011 B2
8069823 Mainini et al. Dec 2011 B2
8098164 Gerig et al. Jan 2012 B2
8159355 Gerig et al. Apr 2012 B2
8161915 Kim Apr 2012 B2
8185345 Mainini May 2012 B2
8232909 Kroeger et al. Jul 2012 B2
8240085 Hill Aug 2012 B2
8269504 Gerig Sep 2012 B2
8274396 Gurley et al. Sep 2012 B2
8297233 Rich et al. Oct 2012 B2
8342134 Lee et al. Jan 2013 B2
8342135 Peinetti et al. Jan 2013 B2
8430064 Groh et al. Apr 2013 B2
8436735 Mainini et al. May 2013 B2
8447510 Fitzpatrick et al. May 2013 B2
8451130 Mainini May 2013 B2
8456296 Piltonen et al. Jun 2013 B2
8483262 Mainini et al. Jul 2013 B2
8714113 Lee, IV et al. May 2014 B2
8715824 Rawlings et al. May 2014 B2
8736499 Goetzl et al. May 2014 B2
8779925 Rich et al. Jul 2014 B2
8803692 Goetzl et al. Aug 2014 B2
8807089 Brown et al. Aug 2014 B2
8823513 Jameson et al. Sep 2014 B2
8854215 Ellis et al. Oct 2014 B1
8866605 Gibson Oct 2014 B2
8908034 Bordonaro Dec 2014 B2
8917172 Charych Dec 2014 B2
8947240 Mainini Feb 2015 B2
8967085 Gillis et al. Mar 2015 B2
9035773 Petersen et al. May 2015 B2
9125380 Deutsch Sep 2015 B2
9131660 Womble Sep 2015 B2
9186091 Mainini et al. Nov 2015 B2
9204251 Mendelson et al. Dec 2015 B1
9307745 Mainini Apr 2016 B2
9861076 Rochelle et al. Jan 2018 B2
10514439 Seltzer Dec 2019 B2
20020010390 Guice et al. Jan 2002 A1
20020015094 Kuwano et al. Feb 2002 A1
20020036569 Martin Mar 2002 A1
20020092481 Spooner Jul 2002 A1
20020103610 Bachmann et al. Aug 2002 A1
20020196151 Troxler Dec 2002 A1
20030034887 Crabtree et al. Feb 2003 A1
20030035051 Cho et al. Feb 2003 A1
20030116099 Kim et al. Jun 2003 A1
20030154928 Lee et al. Aug 2003 A1
20030169207 Beigel et al. Sep 2003 A1
20030179140 Patterson et al. Sep 2003 A1
20030218539 Hight Nov 2003 A1
20040108939 Giunta Jun 2004 A1
20040162875 Brown Aug 2004 A1
20050000469 Giunta et al. Jan 2005 A1
20050007251 Crabtree et al. Jan 2005 A1
20050020279 Markhovsky et al. Jan 2005 A1
20050035865 Brennan et al. Feb 2005 A1
20050059909 Burgess Mar 2005 A1
20050066912 Korbitz et al. Mar 2005 A1
20050081797 Laitinen et al. Apr 2005 A1
20050139169 So et al. Jun 2005 A1
20050145196 Crist et al. Jul 2005 A1
20050145198 Crist et al. Jul 2005 A1
20050145200 Napolez et al. Jul 2005 A1
20050172912 Crist et al. Aug 2005 A1
20050217606 Lee et al. Oct 2005 A1
20050231353 Dipoala et al. Oct 2005 A1
20050235924 Lee, IV et al. Oct 2005 A1
20050258715 Schlabach et al. Nov 2005 A1
20050263106 Steinbacher Dec 2005 A1
20050280546 Ganley et al. Dec 2005 A1
20050288007 Benco et al. Dec 2005 A1
20060000015 Duncan Jan 2006 A1
20060011145 Kates et al. Jan 2006 A1
20060027185 Troxler et al. Feb 2006 A1
20060092676 Liptak et al. May 2006 A1
20060102100 Becker et al. May 2006 A1
20060102101 Kim May 2006 A1
20060112901 Gomez Jun 2006 A1
20060191491 Nottingham et al. Aug 2006 A1
20060196445 Kates Sep 2006 A1
20060197672 Talamas, Jr. et al. Sep 2006 A1
20060202818 Greenberg et al. Sep 2006 A1
20070011339 Brown Jan 2007 A1
20070103296 Paessel et al. May 2007 A1
20070197878 Shklarski Aug 2007 A1
20070204803 Ramsay Sep 2007 A1
20070204804 Swanson et al. Sep 2007 A1
20070209604 Groh et al. Sep 2007 A1
20070249470 Niva et al. Oct 2007 A1
20070266959 Brooks et al. Nov 2007 A1
20080004539 Ross Jan 2008 A1
20080017133 Moore Jan 2008 A1
20080036610 Hokuf et al. Feb 2008 A1
20080055154 Martucci et al. Mar 2008 A1
20080055155 Hensley et al. Mar 2008 A1
20080058670 Mainini et al. Mar 2008 A1
20080061978 Huang Mar 2008 A1
20080061990 Milnes et al. Mar 2008 A1
20080119757 Winter May 2008 A1
20080129457 Ritter et al. Jun 2008 A1
20080141949 Taylor Jun 2008 A1
20080143516 Mock et al. Jun 2008 A1
20080156277 Mainini et al. Jul 2008 A1
20080163827 Goetzl Jul 2008 A1
20080163829 Lee Jul 2008 A1
20080168949 Belcher et al. Jul 2008 A1
20080168950 Moore et al. Jul 2008 A1
20080186167 Ramachandra Aug 2008 A1
20080186197 Rochelle et al. Aug 2008 A1
20080204322 Oswald et al. Aug 2008 A1
20080216766 Martin et al. Sep 2008 A1
20080236514 Johnson et al. Oct 2008 A1
20080252527 Garcia Oct 2008 A1
20080272908 Boyd Nov 2008 A1
20090000566 Kim Jan 2009 A1
20090002188 Greenberg Jan 2009 A1
20090012355 Lin Jan 2009 A1
20090020002 Williams et al. Jan 2009 A1
20090025651 Lalor Jan 2009 A1
20090031966 Kates Feb 2009 A1
20090061772 Moon et al. Mar 2009 A1
20090082830 Folkerts et al. Mar 2009 A1
20090102668 Thompson et al. Apr 2009 A1
20090112284 Smith et al. Apr 2009 A1
20090224909 Derrick et al. Sep 2009 A1
20090239586 Boeve et al. Sep 2009 A1
20090289785 Leonard Nov 2009 A1
20090289844 Palsgrove et al. Nov 2009 A1
20100008011 Ogram Jan 2010 A1
20100033339 Gurley et al. Feb 2010 A1
20100047119 Cressy Feb 2010 A1
20100049364 Landry et al. Feb 2010 A1
20100050954 Lee, IV et al. Mar 2010 A1
20100107985 O'Hare May 2010 A1
20100139576 Kim et al. Jun 2010 A1
20100154721 Gerig et al. Jun 2010 A1
20100231391 Dror et al. Sep 2010 A1
20100238022 Au et al. Sep 2010 A1
20100315241 Jow Dec 2010 A1
20110140967 Lopez et al. Jun 2011 A1
20120000431 Khoshkish et al. Jan 2012 A1
20120006282 Kates Jan 2012 A1
20120037088 Altenhofen Feb 2012 A1
20120078139 Aldridge et al. Mar 2012 A1
20120132151 Touchton et al. May 2012 A1
20120165012 Fischer et al. Jun 2012 A1
20120188370 Bordonaro Jul 2012 A1
20120236688 Spencer et al. Sep 2012 A1
20120312250 Jesurum Dec 2012 A1
20130099920 Song et al. Apr 2013 A1
20130099922 Lohbihler Apr 2013 A1
20130141237 Goetzl et al. Jun 2013 A1
20130157564 Curtis et al. Jun 2013 A1
20130169441 Wilson Jul 2013 A1
20130298846 Mainini Nov 2013 A1
20130321159 Schofield et al. Dec 2013 A1
20140020635 Sayers et al. Jan 2014 A1
20140053788 Riddell Feb 2014 A1
20140062695 Rosen et al. Mar 2014 A1
20140069350 Riddell Mar 2014 A1
20140073939 Rodriguez-Llorente et al. Mar 2014 A1
20140120943 Shima May 2014 A1
20140123912 Menkes et al. May 2014 A1
20140132608 Mund et al. May 2014 A1
20140174376 Touchton et al. Jun 2014 A1
20140228649 Rayner et al. Aug 2014 A1
20140228927 Ahmad et al. Aug 2014 A1
20140253368 Holder Sep 2014 A1
20140253389 Beauregard Sep 2014 A1
20140261235 Rich et al. Sep 2014 A1
20140267299 Couse Sep 2014 A1
20140275824 Couse et al. Sep 2014 A1
20140276278 Smith et al. Sep 2014 A1
20140307888 Alderson et al. Oct 2014 A1
20140320347 Rochelle et al. Oct 2014 A1
20140343599 Smith et al. Nov 2014 A1
20150040840 Muetzel et al. Feb 2015 A1
20150043744 Lagodzinski et al. Feb 2015 A1
20150053144 Bianchi et al. Feb 2015 A1
20150075446 Hu Mar 2015 A1
20150080013 Venkatraman et al. Mar 2015 A1
20150107531 Golden Apr 2015 A1
20150149111 Kelly et al. May 2015 A1
20150163412 Holley et al. Jun 2015 A1
20150172872 Alsehly et al. Jun 2015 A1
20150173327 Gerig et al. Jun 2015 A1
20150199490 Iancu et al. Jul 2015 A1
20150223013 Park et al. Aug 2015 A1
20150289111 Ozkan et al. Oct 2015 A1
20150350848 Eramian Dec 2015 A1
20150358768 Luna et al. Dec 2015 A1
20160015005 Brown, Jr. et al. Jan 2016 A1
20160021506 Bonge, Jr. Jan 2016 A1
20160021850 Stapelfeld et al. Jan 2016 A1
20160029466 Demao et al. Jan 2016 A1
20160044444 Rattner et al. Feb 2016 A1
20160084801 Robinson et al. Mar 2016 A1
20160094419 Peacock et al. Mar 2016 A1
20160102879 Guest et al. Apr 2016 A1
20160150362 Shaprio et al. May 2016 A1
20160174099 Goldfain Jun 2016 A1
20160178392 Goldfain Jun 2016 A1
20160187454 Orman et al. Jun 2016 A1
20160253987 Chattell Sep 2016 A1
20160335917 Lydecker et al. Nov 2016 A1
20160363664 Mindell et al. Dec 2016 A1
20170212205 Bialer Jul 2017 A1
20170323630 Stickney et al. Nov 2017 A1
20180027772 Gordon et al. Feb 2018 A1
20180077509 Jones et al. Mar 2018 A1
20180078735 Dalgleish et al. Mar 2018 A1
20180094451 Peter et al. Apr 2018 A1
20180188351 Jones et al. Jul 2018 A1
20180210704 Jones et al. Jul 2018 A1
20180234134 Tang et al. Aug 2018 A1
20180235182 Bocknek Aug 2018 A1
20180315262 Love et al. Nov 2018 A1
20190013003 Baughman et al. Jan 2019 A1
20190110430 Badiou Apr 2019 A1
20190165832 Khanduri et al. May 2019 A1
Foreign Referenced Citations (17)
Number Date Country
101112181 Jan 2008 CN
101937015 Jan 2011 CN
101112181 Nov 2012 CN
102793568 Dec 2014 CN
H0974774 Mar 1997 JP
20130128704 Nov 2013 KR
WO-02060240 Feb 2003 WO
WO-2006000015 Jan 2006 WO
WO-2008085812 Jul 2008 WO
WO-2008140992 Nov 2008 WO
WO-2009105243 Aug 2009 WO
WO-2009106896 Sep 2009 WO
WO-2011055004 May 2011 WO
WO-2011136816 Nov 2011 WO
WO-2012122607 Sep 2012 WO
WO-2015015047 Feb 2015 WO
WO-2016204799 Dec 2016 WO
Non-Patent Literature Citations (25)
Entry
Baba A.I., et al., “Calibrating Time of Flight in Two Way Ranging,” IEEE Xplore Digital Library, Dec. 2011, pp. 393-397.
Eileen—How to Protect Your Dog From Loud and Scary Sounds (Year: 2013).
Extended European Search Report for Application No. EP17180645, dated May 9, 2018, 7 pages.
Extended European Search Report for European Application No. 11784149.4 dated Nov. 17, 2017, 7 pages.
Extended European Search Report for European Application No. 15735439.0 dated Oct. 18, 2017, 9 pages.
Extended European Search Report for European Application No. 15895839.7 dated Oct. 9, 2018, 5 pages.
Extended European Search Report for European Application No. 17162289.7 dated Aug. 31, 2017, 7 pages.
High Tech Products, Inc: “Human Contain Model X-10 Rechargeable Muti-function Electronic Dog Fence Ultra-system”, Internet citation, Retrieved from the Internet: URL:http://web.archive.org/web/20120112221915/http://hightechpet.com/user_Manuals/HC%20X-10_Press.pdf retrieved on Apr. 10, 2017], Apr. 28, 2012, pp. 1-32, XP008184171.
International Preliminary Report for Patentability Chapter II for International Application No. PCT/US2014/024875 dated Mar. 12, 2015, 17 pages.
International Preliminary Report on Patentability for Application No. PCT/US2015/043653 dated Dec. 19, 2017, 14 pages.
International Search Report and Written Opinion for Application No. PCT/US2018/013737 dated Mar. 7, 2018, 8 pages.
International Search Report and Written Opinion for Application No. PCT/US2018/013738 dated Mar. 20, 2018, 6 pages.
International Search Report and Written Opinion for Application No. PCT/US2018/013740 dated Mar. 20, 2018, 6 pages.
International Search Report and Written Opinion for Application No. PCT/US2018/019887 dated May 8, 2018, 10 pages.
International Search Report and Written Opinion for International Application No. PCT/US2014/024875 dated Jun. 27, 2014, 12 pages.
International Search Report for International Application No. PCT/US2014/020344 dated Jun. 5, 2014, 2 pages.
International Search Report for International Application No. PCT/US2014/066650 dated Feb. 19, 2015, 3 pages (Outgoing).
International Search Report for International Application No. PCT/US2015/010864, Form PCT/ISA/210 dated Apr. 13, 2015, 2 pages.
International Search Report for International Application No. PCT/US2015/043653, Form PCT/ISA/210 dated Oct. 23, 2015, 2 pages.
Notification of Transmittal of the International Search Report and the Written Opinion of the International Searching Authority for International Application No. PCT/US2015/043653, Form PCT/ISA/220 dated Oct. 23, 2015, 1 page.
Notification of Transmittal of the International Search Report and Written Opinion for the International Application No. PCT/US2014/066650 dated Feb. 19, 2015, 1 page.
Welch et al., “An Introduction to the Kalman Filter,” Department of Computer Science, Jul. 24, 2006, pp. 1-16.
Written Opinion for International Application No. PCT/US2014/066650 dated Feb. 19, 2015, 15 pages(outgoing).
Written Opinion for International Application No. PCT/US2015/043653, Form PCT/ISA/237 dated Oct. 23, 2015, 13 pages.
Written Opinion of the International Application No. PCT/US2015/010864, Form PCT/ISA/237 dated Apr. 13, 2015, 6 pages.
Related Publications (1)
Number Date Country
20200225312 A1 Jul 2020 US
Provisional Applications (1)
Number Date Country
62599248 Dec 2017 US
Continuations (1)
Number Date Country
Parent 16003876 Jun 2018 US
Child 16715420 US