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NL2036436B1 - Method for determining a position range of a third-party drone or a transmitter of a control device of the third-party drone - Google Patents

Method for determining a position range of a third-party drone or a transmitter of a control device of the third-party drone

Info

Publication number
NL2036436B1
NL2036436B1 NL2036436A NL2036436A NL2036436B1 NL 2036436 B1 NL2036436 B1 NL 2036436B1 NL 2036436 A NL2036436 A NL 2036436A NL 2036436 A NL2036436 A NL 2036436A NL 2036436 B1 NL2036436 B1 NL 2036436B1
Authority
NL
Netherlands
Prior art keywords
drone
sensor
range
solid angle
determined
Prior art date
Application number
NL2036436A
Other languages
Dutch (nl)
Other versions
NL2036436A (en
Inventor
Niesen Klaus
Bratz Kurt
Brinkmeyer Joerg
Original Assignee
Bosch Gmbh Robert
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Bosch Gmbh Robert filed Critical Bosch Gmbh Robert
Publication of NL2036436A publication Critical patent/NL2036436A/en
Application granted granted Critical
Publication of NL2036436B1 publication Critical patent/NL2036436B1/en

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Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/60Intended control result
    • G05D1/656Interaction with payloads or external entities
    • G05D1/689Pointing payloads towards fixed or moving targets
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO 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
    • G01S5/00Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
    • G01S5/02Position-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
    • G01S5/04Position of source determined by a plurality of spaced direction-finders
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/20Control system inputs
    • G05D1/24Arrangements for determining position or orientation
    • G05D1/243Means capturing signals occurring naturally from the environment, e.g. ambient optical, acoustic, gravitational or magnetic signals
    • GPHYSICS
    • G08SIGNALLING
    • G08GTRAFFIC CONTROL SYSTEMS
    • G08G5/00Traffic control systems for aircraft
    • G08G5/20Arrangements for acquiring, generating, sharing or displaying traffic information
    • G08G5/22Arrangements for acquiring, generating, sharing or displaying traffic information located on the ground
    • GPHYSICS
    • G08SIGNALLING
    • G08GTRAFFIC CONTROL SYSTEMS
    • G08G5/00Traffic control systems for aircraft
    • G08G5/50Navigation or guidance aids
    • G08G5/53Navigation or guidance aids for cruising
    • GPHYSICS
    • G08SIGNALLING
    • G08GTRAFFIC CONTROL SYSTEMS
    • G08G5/00Traffic control systems for aircraft
    • G08G5/50Navigation or guidance aids
    • G08G5/55Navigation or guidance aids for a single aircraft
    • GPHYSICS
    • G08SIGNALLING
    • G08GTRAFFIC CONTROL SYSTEMS
    • G08G5/00Traffic control systems for aircraft
    • G08G5/70Arrangements for monitoring traffic-related situations or conditions
    • G08G5/72Arrangements for monitoring traffic-related situations or conditions for monitoring traffic
    • G08G5/727Arrangements for monitoring traffic-related situations or conditions for monitoring traffic from a ground station
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO 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
    • G01S2205/00Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
    • G01S2205/01Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations specially adapted for specific applications
    • G01S2205/03Airborne
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D2105/00Specific applications of the controlled vehicles
    • G05D2105/80Specific applications of the controlled vehicles for information gathering, e.g. for academic research
    • G05D2105/85Specific applications of the controlled vehicles for information gathering, e.g. for academic research for patrolling or reconnaissance for police, security or military applications
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D2107/00Specific environments of the controlled vehicles
    • G05D2107/10Outdoor regulated spaces
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D2109/00Types of controlled vehicles
    • G05D2109/20Aircraft, e.g. drones
    • G05D2109/25Rotorcrafts
    • G05D2109/254Flying platforms, e.g. multicopters
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D2111/00Details of signals used for control of position, course, altitude or attitude of land, water, air or space vehicles
    • G05D2111/30Radio signals
    • GPHYSICS
    • G08SIGNALLING
    • G08GTRAFFIC CONTROL SYSTEMS
    • G08G5/00Traffic control systems for aircraft
    • G08G5/50Navigation or guidance aids
    • G08G5/57Navigation or guidance aids for unmanned aircraft
    • GPHYSICS
    • G08SIGNALLING
    • G08GTRAFFIC CONTROL SYSTEMS
    • G08G5/00Traffic control systems for aircraft
    • G08G5/50Navigation or guidance aids
    • G08G5/59Navigation or guidance aids in accordance with predefined flight zones, e.g. to avoid prohibited zones

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

The invention relates to a method and system for determining a position range (30, 32) of a third-party drone (20) or of a transmitter (44) of a control device of the third-party drone, wherein a transmission signal of the third- party drone or of the transmitter is detected with a first radio frequency, RF, sensor which is attached to a sensor drone (10), wherein a first solid angle range (24, 26) starting from a first detection position located on a flight path of the sensor drone (10) is determined based on the detected transmission signal, and wherein the position range (30, 32) is narrowed down (120) to the first solid angle range or is determined as the first solid angle range or as a subrange of the first solid angle range, and/or wherein the position range is determined as a function of the detected transmission signal. (Figure 1D)

Description

P136309NL00
Title: Method for determining a position range of a third-party drone or a transmitter of a control device of the third-party drone
The present invention relates to a method for determining a position range of a third-party drone or a transmitter of a control device of the third-party drone and a system for carrying it out.
Background of the invention
Drones, especially in the form of so-called multicopters, are becoming increasingly widespread. These drones pose a potential security risk for sensitive areas or objects, such as airports or aircraft, buildings, crowds of people, production facilities, military installations, nuclear power plants and the like. For example, a collision (whether intentional or unintentional) with an aircraft can cause considerable damage to the aircraft.
Commercially available drones can weigh between approx. 100 g and approx. 25 kg or more and reach speeds of up to 50 km/h to 100 km/h, depending on the type. At the same time, the maximum flight altitude can be one kilometre or more. The maximum payload of such drones can be around 1 kg to 5 kg or around a quarter of their own weight. Typical ranges can be several kilometres.
US 10 866 597 B1 relates to systems and methods for detecting and intercepting drones in order to counter dangers posed by drones.
Disclosure of the invention
According to the invention, a method for determining or narrowing down a position range of a third-party drone or a transmitter of a control device of the third-party drone and a system with the features of the independent patent claims are proposed. Advantageous embodiments are the subject of the dependent claims and the following description.
The invention utilises the measure of using a sensor drone with an RF sensor (RF: radio frequency; approximately 3 kHz to 300 GHz) at a detection position on a flight path of the sensor drone to determine a solid angle range emanating from the sensor drone or the RF sensor, in which the third-party drone is located, and to constrict or narrow down a position range of the third-party drone or a transmitter of a control device of the third-party drone to the specific solid angle range. This procedure is expedient because the detection position or the flight path can be freely selected and, in particular, can also be changed, e.g. can be selected at a height at which interference of RF signals by topography and vegetation does not occur, and thus the narrowing of the position range can be improved compared to an estimation of the position of the third-party drone by a fixed drone detection system.
The sensor drone is set up to detect at least one RF signal by means of the
RF sensor, which 1s attached to the sensor drone, and to determine a solid angle range in which a transmitter of the RF signal is located as seen from the sensor drone or from the RF sensor. In particular, the RF sensor is tuned to frequency ranges or bands in which RF control signals are typically transmitted by control devices for drones or in which drones transmit data to the control devices, for example in the GHz range, such as 2.4 GHz or 5.8
GHz.
RF sensors are sensors that are set up to determine the direction or a corresponding solid angle range (e.g. by using antennas with directional characteristics) of RF signals. Typically, the power density or energy flow of the RF signal is determined for this purpose. In particular, the term RF sensor does not refer to RF receivers used on drones to receive RF control signals. However, it is possible for an RF sensor to also act as an RF receiver,
By providing an input signal with an exact position (e.g. GNSS) and an exact time stamp (e.g. DCF 77), the position of the transmitter can be determined from three of these transit time values using a triangulation method, i.e. here the position of the third-party drone, if it 1s transmitting communication signals, and the remote control system (control device) of the third-party drone on the ground. At least three HF sensors should be used for triangulation, for example. More HF sensors lead to a higher accuracy of the position.
Further advantages and embodiments of the invention are shown in the description and the accompanying drawing.
The invention is illustrated schematically in the drawing by means of embodiment examples and is described below with reference to the drawing.
Brief description of the drawings
Figures 1A to 1F show an example of the procedure for narrowing down a position range of a third-party drone or a transmitter of a control device of the third-party drone.
Figure 2 shows a situation in which the sensor drone is in the immediate vicinity of the transmitter and the operator 46 of the control device of the third-party drone.
Figures 3A and 3B illustrate the use of two sensor drones.
Figure 4 shows a flow chart of the method for determining a position range of a third-party drone or a transmitter of a control device of the third-party drone.
Embodiment(s) of the invention
Figures 1A-1F show an example of the procedure for narrowing a position range of a third-party drone and/or a transmitter of a control device of the third-party drone.
Figures 1A-1F each show a sensitive air zone 2, i.e. a defined air zone in which unknown drones or third-party drones are not desired. The air zone 2 can be defined in a suitable manner, e.g. so that it surrounds an object 4 to be protected, such as an airport. In particular, the air zone 2 can be an air zone into which unauthorised entry by drones or other aircraft is not permitted due to legal standards. The figures show, for example, a third- party drone 20, which is located outside the defined air zone 2 in Figure 1A.
The system shown comprises a drone detection system 12, at least one sensor drone 10, in Figure 1A for example in a parking position, and preferably a guidance system 14. The guidance system 14 is in particular set up to evaluate and/or summarise data from the drone detection system and/or the sensor drone and/or to transmit data and/or control commands to the sensor drone.
The drone detection system 12 is fixedly positioned relative to the sensitive (defined) air zone 2, e.g. standing on the ground inside or outside the air zone or attached to or on a building, and is set up to detect drones, in particular multicopters, within the sensitive air zone 2. In general, of 5 course, drones outside the air zone and/or other objects are also detected, 1.e. the detection range of the drone detection system 12 generally extends beyond the sensitive air zone 2.
The drone detection system 12 is formed here, for example, by two fixed (i.e. with a fixed position) RF sensors 18 (radio frequency sensor). In general, any number of fixed RF sensors can be provided, e.g. also more than two fixed RF sensors or no fixed RF sensor if other sensors are used. RF sensors can be used to detect drones and/or drone control devices, as both drones and drone control devices typically have an RF transmitter.
In general, the drone detection system 12 comprises one or more sensors that detect drones and generally other objects in the air zone 2, in particular at least one radar sensor and/or at least one lidar sensor (light detection and ranging, also known as light imaging, detection and ranging) and/or at least one RF sensor (radio frequency sensor) and/or at least one camera (optical and/or infrared) and/or at least one microphone. Preferably, the drone detection system is set up in such a way that it is possible to distinguish drones from other objects (e.g. birds). For this purpose, the so-called “micro-
Doppler effect" can be used with radar sensors or lidar sensors. This utilises the fact that vibrating and/or rotating elements on the detected object (in particular the propeller of a multicopter) lead to a modulation, i.e. frequency modulation due to the Doppler effect, of the radar signal or lidar signal, which is imposed on the radar signal in addition to the frequency shift due to the speed of the detected object. Such a modulation can be recognised by evaluating the radar signal or lidar signal and thus a drone can be distinguished from a bird, for example. It is also possible to recognise drones on the basis of the noise caused by their propellers. Camera images can also be used to distinguish drones from other objects. For example, an image recognition system could be used, such as a neural network (or an algorithm based on machine learning), which has been trained accordingly using existing camera images of drones and other objects.
The drone detection system 12 is set up to determine position data of detected objects, in particular of detected drones. In general, sensors of the drone detection system 12 cannot determine the exact position of drones.
For example, RF sensors can only determine a direction or a solid angle range within which an RF transmitter is located, while the distance cannot be determined precisely. Figure 1B, for example, shows a situation in which the third-party drone 20 is detected by the fixed RF sensors 18 as it enters the defined air zone 2, whereby a solid angle range 22 is shown for each of the two RF sensors, within which the third-party drone 20 is located based on the RF signals detected by the respective RF sensor. These solid angle ranges 22 indicate the probable location of the third-party drone, as there is only a certain degree of measurement accuracy and/or interference, such as signal reflections from buildings, can occur. The solid angle ranges 22 can be used to narrow down or constrict the position of the third-party drone 20 to the location range 31, namely the intersection of the solid angle ranges.
As soon as the location range 31 of the third-party drone 20 determined by the RF sensors 18 (or other sensors of the drone detection system) is at least partially in the defined air zone 2, it is assumed that the third-party drone 20 has entered the air zone 2. In this case, the sensor drone 10 can be started, as shown in Figure 1B. In general, the sensor drone 10 may already be flying in the air, i.e. it may have been launched at an earlier point in time.
Target data or trajectory data, which indicate the direction or trajectory 1n which the sensor drone should fly, can be determined, for example, based on the already known position within the location range 31 where the third- party drone is located and can be transmitted to a control unit or drone control unit of the sensor drone 10 and/or the guidance system 14. Based on the target data or trajectory data, a corresponding flight path of the sensor drone can be determined by controlling the sensor drone. The drone control unit can be or include an automatic control unit, i.e. the sensor drone is at least partially controlled automatically, and/or be or include a remote control unit for a (human) user, i.e. the sensor drone is remotely controlled by the user, who makes control inputs by means of operating elements of the remote control unit (in particular possible via radio as well as via mobile radio networks or direct link). For example, a corresponding computer program for the remote control unit can be executed in a computer in the guidance system. The remote control unit can, for example, be provided in the guidance system 14 and/or be a portable remote control unit. The automatic control unit can, for example, be implemented in a computer unit in the sensor drone itself and/or in a computer unit in the guidance system (by means of corresponding computer programs).
In Figure 1C, the sensor drone 10 is located at a position referred to as the detection position, which is located on the flight path of the sensor drone, i.e. on the flight path of the sensor drone resulting from the target data or trajectory data. The detection position can be at a predetermined height, for example. This height can be determined in such a way that it can be assumed that RF signals from the third-party drone to the sensor drone are not disturbed by buildings, trees or the like. An RF sensor is attached to the sensor drone 10, which 1s also used to detect the third-party drone 20 or its
RF transmitter. A solid angle range 24 is therefore determined, within which the third-party drone 20 is (probably) located as seen from the sensor drone 10. The position of the third-party drone 20 can therefore be narrowed down or constricted to the solid angle range 24. In addition, the solid angle ranges 22 within which the third-party drone 10 is located as seen from the fixed RF sensors can be taken into account, so that overall the position of the third-party drone 20 can be narrowed down to the position range 30 shown as a dashed line. Due to the free and, in particular, less interference- prone positioning of the sensor drone 10, a considerable improvement in the position determination of the third-party drone 20 can be achieved, i.e. a reduction in the specific position range 30 within which the third-party drone 20 is probably located (based on the detection by RF sensors) can be achieved.
Figure 1D shows a situation corresponding to Figure 1C, 1.e. the third-party drone 20 is detected by the sensor drone 10 or its RF sensor from a first detection position (which may be the same as the detection position in
Figure 1C or may be a different detection position) located on the flight path of the sensor drone 10, so that the position of the third-party drone 20 can be narrowed down to a (first) solid angle range 24. For the sake of clarity, in
Figure 1D, as in Figures 1E and 1F, not all reference signs from Figure 1C have been repeated.
In addition or as an alternative to Figure 1C, in Figure 1D the transmitter 44 of a control device of the third-party drone 20, which is held for example by an operator 46 of the third-party drone, is detected by the sensor drone 10 or its RF sensor, respectively. Accordingly, a position of the transmitter 44 of the control device can be narrowed down to a (first) solid angle range 26 in which the transmitter 44 of the control device is located as seen from the sensor drone 10. More precisely, from the point of view of the sensor drone 10, it is initially a transmitter of a potential control device of the third-party drone 20, since the sensor drone generally cannot decide whether it is the transmitter 44 of the control device of the third-party drone 20 or any other RF transmitter. In particular, an assignment of the detected RF signals is possible if they contain identification information, e.g. a MAC address and/or a remote identification described below. Other (physical) properties (e.g. frequency) of the RF signals can also be analysed to enable assignment. If, as described below, for example, several solid angle ranges are determined, those that were determined based on associated RF signals are taken into account.
The position range of the third-party drone or its control device can also (additionally or alternatively) be determined as a function of the detected transmission signal (RF signal), for example by analysing a remote identification or remote ID transmitted with it or in it, which can also be regarded as identification information. For example, information is transmitted that includes the identification of an unmanned aerial vehicle (UAV) (in this case a drone or third-party drone). Remote identification can include one or more of the following data: unmanned aircraft system (UAS) operator number, serial number, position data, current flight altitude, flight direction, flight speed, starting point of the drone. Direct remote identification means a system that ensures the local transmission of information about an unmanned aircraft in operation and also includes the identification of the unmanned aircraft so that this information can be retrieved without physical access to the unmanned aircraft.
Furthermore, trees 50 and a lake 52, which are located in an exemplary environment of the air zone 2, are shown. The topology of the environment can be taken into account so that, assuming that the transmitter 44 is located approximately at ground level, the dashed position range 32 for the transmitter 44 can be determined (for example as the intersection of the first solid angle range 26 and a height range above the ground, e.g. a height range with a height of 5 m or 10 m).
The situation depicted in Figure 1E essentially corresponds to that depicted in Figure 1D, with the difference that the sensor drone 10 is at a new (second) detection position. The second detection position can, for example, be determined based on the first solid angle range 26, i.e. the target data or trajectory data is adjusted accordingly so that a desired second detection position is on the flight path of the sensor drone. For example, the solid angle range can be followed so that the second detection position is within the first solid angle range 26 in order to reduce the distance to the transmitter. Alternatively, the second detection position could be outside the first solid angle range 26 to allow triangulation of the transmitter (which is assumed not to change its position at all or only slowly).
Based on the second detection position, a second solid angle range 28 in which the transmitter 44 is (probably) located can be determined by the sensor drone 10 or its RF sensor, respectively. If, as shown, the second detection position is located in the first solid angle range, the position range 32m which the transmitter 44 is (probably) located can be reduced compared to that in Figure 1C, for example by taking topological information into account. If, as not shown, the second detection position is located outside the first solid angle range, the intersection of the first and second solid angle ranges can be formed, for example, so that triangulation is possible in principle Gf the second detection position is suitably selected).
The RF sensor of the sensor drone can detect RF signals continuously, for example, so that solid angle ranges in which a transmitter (of the third- party drone and/or the control device of the third-party drone) is located as seen from the respective position of the sensor drone are determined continuously (continuously or at certain time intervals, which are determined, for example, by the computing unit used to analyse the RF signals) on the flight path of the sensor drone. In general, therefore, a large number of detection positions and associated solid angle ranges can be determined. When determining the position range in which the transmitter is located, all or part of this plurality of detection positions and associated solid angle ranges can be taken into account, i.e. the position range can be formed as an intersection of all or part of this plurality of solid angle ranges (as seen from the respective detection positions) or, insofar as other information, e.g. of the fixed RF sensors, is used, can be narrowed down to this intersection. How many and which of this plurality are taken into account can be determined, for example, depending on the distance between the detection positions and/or on the available computing power and/or on whether it is assumed that the transmitter is moving. The first and second detection positions shown in Figures 1D and 1E represent examples of this generally plurality of detection positions. The RF sensor of the sensor drone may, but need not, continuously detect RF signals, wherein if RF signals are not continuously detected, RF signals are at least detected when the sensor drone 1s at the detection positions.
The situation shown in Figure 1F essentially corresponds to that shown in
Figure 1E, with the difference that the fixed RF sensors 18 additionally determine respective (third) solid angle ranges 23 within which the transmitter 44 of the control device of the third-party drone 20 is located.
The position range 32, in which the transmitter 44 is (probably) located, can then be narrowed down to the intersection of the three solid angle ranges (second solid angle range 28, solid angle ranges 23 of the two fixed RF sensors 18).
Figure 2 shows a situation in which the sensor drone 10 is located in the immediate vicinity of the transmitter 44 and the operator 46 of the control device of the third-party drone, e.g. at a third detection position on the flight path of the sensor drone, for example as a result of a determination of the position range of the transmitter 44 of the control device of the third-party drone 20. The sensor drone 10 or its RF sensor, respectively, can also be used to determine solid angle ranges (e.g. the solid angle range 29 shown) within which the third-party drone 20 or the transmitter 44 are located. The third-party drone 20 is, for example, approaching a landing site 66.
A camera 62 can be attached to the sensor drone 10, with which images of the third-party drone 10 and/or the control device or the operator 46 can be taken, in particular in order to determine their position in relation to the surroundings and thus further narrow down the corresponding position ranges. A loudspeaker 64 can also be attached to the sensor drone 10, with which an announcement can be made, for example to inform the operator 46 of the unauthorised entry into the defined air zone 2.
The sensor drone 10 may remain at this location, for example, until members of a competent authority, such as the police, who have been informed via the guidance system 14, for example, can reach this location via a nearby road 68 using a motor vehicle 70.
Figures 3A and 3B illustrate the use of two sensor drones 10 flying on different trajectories. In Figure 3A, which essentially corresponds to the situation in Figures 1D and 1E, the two sensor drones 10 are at different detection positions, so that two solid angle ranges 29 can be determined by the data from the sensor drones 10 or their RF sensors, respectively, and the position of the transmitter 44 of the control device of the third-party drone 20 can be narrowed down to the intersection of these two solid angle ranges 29 (position range 32).
In the situation illustrated in Figure 3B, two third-party drones 20a, 20b, which are controlled by two control devices with transmitters 44a, 44b by operators at different locations, have also entered the defined air zone 2. A sensor drone 10 can determine a solid angle range 24a, in which a first of the third-party drones 20a is located, a solid angle range 29a, in which the transmitter 44a of the control device of the first third-party drone 20a is located, and a solid angle range 29b, in which the transmitter 44b of the control device of the other, second third-party drone 20b is located.
Furthermore, the sensor drone 10 can determine a solid angle range in which a second of the third-party drones 20b is located (not shown for the sake of clarity). The other sensor drone 10 can determine a solid angle range 24b in which the second third-party drone 20b is located, a solid angle range 29b in which the transmitter 44b of the control device of the second third- party drone 20b is located, and a solid angle range 29a in which the transmitter 44a of the control device of the first third-party drone 20a is located. Furthermore, the other sensor drone 10 can determine a solid angle range in which a first of the third-party drones 20a is located (not shown for the sake of clarity). The positions of the third-party drones 204, 20b or the transmitters 44a, 44b can be narrowed down accordingly by the respective solid angle ranges.
Figure 4 shows a flow chart of the method for determining a position range of a third-party drone or a transmitter of a control device of the third-party drone.
In optional step 100, the intrusion of a third-party drone into a defined air zone 1s detected, for example by a drone detection system, and a sensor drone with an RF sensor attached to it is launched (see Figure 1B).
In step 110, the sensor drone is controlled to determine, at a first detection position on a flight path of the sensor drone (on which the sensor drone is approximately controlled to fly), a first solid angle range in which the third- party drone or a transmitter of a control device of the third-party drone is located as seen from the first detection position by detecting and evaluating
RF signals (transmission signal).
In step 120, the position of the third-party drone or of the transmitter of the control device is narrowed down or constricted to a position range corresponding to the first solid angle range or narrowed down to the first solid angle range. In particular, the position range may be determined to be equal to the solid angle range, for example if no further information about the location of the third-party drone or the transmitter of the control device is available, or, if such further information is available, the position range may be determined as an intersection of the solid angle range and a location range derived from this information, i.e. as a subrange of the solid angle range. In general, the position range is therefore determined as being equal to the solid angle range or as a subrange of the solid angle range. The position range can be determined as a function of the RF signal that transmits a remote identification or remote ID, for example.
In the optional step 130, the sensor drone is controlled to determine a second solid angle range, in which the third-party drone or the transmitter of the control device of the third-party drone is located, at a second detection position on the flight path of the sensor drone by detecting and analysing
RF signals (transmission signal). The flight path and/or the second detection position can be determined, for example, based on the first solid angle range and/or other information.
In the optional step 140, the position of the third-party drone or of the transmitter of the control device is narrowed down to the position range corresponding to or to the second solid angle range. In particular, the position range can be determined as the intersection of the first solid angle range with the second solid angle range and possibly further information. In order to be able to better allocate solid angle ranges to one another (i.e. allocate solid angle ranges belonging to the same transmitter to one another), identification information contained in the transmission signal and/or a remote identification can be taken into account. The procedure of steps 110 and 120 or 130 and 140 can be repeated as often as desired or continuously. The position range determined during a previous repetition can be taken into account, e.g. as further information (of steps 120 or 140).
In the optional step 150, the sensor drone is controlled (automatically or manually) to fly to a third detection position and, during the flight and/or after reaching the third detection position, to take images of the specific position range using a camera attached to the sensor drone. Such images can be used to narrow down the position range in relation to the surroundings or objects located in the surroundings, such as houses or trees or similar.

Claims (13)

ConclusiesConclusions 1. Werkwijze voor de bepaling van een positiebereik (30, 32) van een vreemde drone (20) of van een zender (44) van een stuurinrichting van de vreemde drone, waarbij een zendsignaal van de vreemde drone respectievelijk van de zender met een eerste hoge-frequentie, HF, -sensor wordt vastgesteld, die aan een sensordrone (10) is aangebracht, waarbij gebaseerd op het vastgestelde zendsignaal een eerste ruimtehoekbereik (24, 26) wtgaande van een eerste registratiepositie, die zich op een vliegroute van de sensordrone (10) bevindt, wordt bepaald, en waarbij het positiebereik (30, 32) waarop het eerste ruimtehoekbereik wordt beperkt (120) respectievelijk als het eerste ruimtehoekbereik of als deelbereik van het eerste ruimtehoekbereik wordt bepaald en/of het positiebereik in afhankelijkheid van het vastgestelde zendsignaal wordt bepaald.1. Method for determining a position range (30, 32) of a foreign drone (20) or of a transmitter (44) of a control device of the foreign drone, wherein a transmission signal of the foreign drone or of the transmitter is determined with a first high-frequency, HF, sensor, which is mounted on a sensor drone (10), wherein a first solid angle range (24, 26) starting from a first registration position, which is located on a flight path of the sensor drone (10), is determined based on the determined transmission signal, and wherein the position range (30, 32) to which the first solid angle range is limited (120) is determined as the first solid angle range or as a sub-range of the first solid angle range, respectively, and/or the position range is determined as a function of the determined transmission signal. 2. Werkwijze volgens conclusie 1, waarbij gebaseerd op het met de eerste HF-sensor vastgestelde zendsignaal ten minste een tweede ruimtehoekbereik (24, 28) uitgaande van ten minste een tweede registratiepositie, die zich op de vliegroute van de sensordrone (10) bevindt, wordt bepaald, en waarbij het positiebereik (30, 32) voorts tot het ten minste ene tweede ruimtehoekbereik wordt beperkt (140).Method according to claim 1, wherein at least a second solid angle range (24, 28) is determined based on the transmission signal determined with the first RF sensor, starting from at least a second registration position located on the flight path of the sensor drone (10), and wherein the position range (30, 32) is further limited (140) to the at least one second solid angle range. 3. Werkwijze volgens conclusie 2, waarbij de vliegroute van de sensordrone na de eerste registratiepositie en/of de ten minste ene tweede registratiepositie gebaseerd op het eerste ruimtehoekbereik (26) en/of gebaseerd op het positiebereik (32) overeenkomstig met de tot nu toe geldende beperking wordt respectievelijk worden bepaald.Method according to claim 2, wherein the flight path of the sensor drone after the first registration position and/or the at least one second registration position is/are determined based on the first solid angle range (26) and/or based on the position range (32) in accordance with the limitation applicable up to now. 4. Werkwijze volgens een der voorgaande conclusies, waarbij het zendsignaal met ten minste een tweede HF-sensor (18), die zich op ten minste een vaste positie bevindt, wordt vastgesteld, waarbij gebaseerd op het met de tweede HF-sensor vastgestelde zendsignaal ten minste een derde ruimtehoekbereik (23) uitgaande van de ten minste ene eerste positie wordt bepaald, en waarbij het positiebereik (32) voorts tot het ten minste ene derde ruimtehoekbereik wordt beperkt.Method according to any one of the preceding claims, wherein the transmit signal is determined with at least a second RF sensor (18) located at at least one fixed position, wherein at least a third solid angle range (23) is determined starting from the at least one first position based on the transmit signal determined with the second RF sensor, and wherein the position range (32) is further limited to the at least one third solid angle range. 5. Werkwijze volgens een der voorgaande conclusies, waarbij in het zendsignaal aanwezige identificatie-informaties en/of eigenschappen van het zendsignaal worden geëvalueerd en waarmee rekening wordt gehouden bij de bepaling respectievelijk beperking van het positiebereik, in het bijzonder voor de toewijzing van een of meer van de bepaalde ruimtehoekbereiken.Method according to any one of the preceding claims, wherein identification information and/or properties of the transmit signal present in the transmit signal are evaluated and taken into account when determining or limiting the position range, in particular for the allocation of one or more of the determined solid angle ranges. 6. Werkwijze volgens een der voorgaande conclusies, waarbij de sensordrone (10) wordt gestuurd om naar ten minste een derde registratiepositie in het positiebereik (32) overeenkomstig met de tot nu toe geldende beperking te vliegen (150), waarbij tijdens de vlucht naar ten minste een derde registratiepositie en/of na het bereiken van de ten minste ene derde registratiepositie een of meer cameraopnamen met een aan de sensordrone aangebrachte camera (62) worden vastgesteld (160).Method according to any one of the preceding claims, wherein the sensor drone (10) is controlled to fly (150) to at least one third registration position in the position range (32) in accordance with the restriction applicable up to now, wherein during the flight to at least one third registration position and/or after reaching the at least one third registration position one or more camera recordings are recorded (160) with a camera (62) mounted on the sensor drone. 7. Werkwijze volgens een der voorgaande conclusies, waarbij, in het bijzonder voor het bepalen van het eerste ruimtehoekbereik (24, 26), door een droneregistratiesysteem (12) wordt herkend, dat de vreemde drone (20) in een gedefinieerd luchtbereik (2) is ingedrongen, waarbij een aanwezigheidsbereik (31) van de vreemde drone en/of van de zender van de stuurinrichting van de vreemde drone door het droneregistratiesysteem wordt bepaald, waarbij de vliegroute van de sensordrone en/of de eerste registratiepositie gebaseerd op het aanwezigheidsbereik van de vreemde drone en/of van de zender van de stuurinrichting van de vreemde drone wordt bepaald.Method according to any one of the preceding claims, wherein, in particular for determining the first solid angle range (24, 26), a drone registration system (12) recognizes that the foreign drone (20) has entered a defined air area (2), wherein a presence range (31) of the foreign drone and/or of the transmitter of the control device of the foreign drone is determined by the drone registration system, wherein the flight path of the sensor drone and/or the first registration position is determined based on the presence range of the foreign drone and/or of the transmitter of the control device of the foreign drone. 8. Werkwijze volgens conclusie 7, waarbij de sensordrone (10) in reactie op het herkennen, dat de vreemde drone in het gedefinieerde luchtbereik 1s ingedrongen, wordt gestart.Method according to claim 7, wherein the sensor drone (10) is started in response to detecting that the foreign drone has entered the defined air range 1s. 9. Werkwijze volgens een der voorgaande conclusies, waarbij een verdere sensordrone (10), waaraan een derde HF-sensor is aangebracht, wordt gestuurd om naar een vierde registratiepositie te vliegen, waarbij een zendsignaal van de vreemde drone respectievelijk van de zender met de derde HF-sensor wordt vastgesteld, waarbij gebaseerd op het vastgestelde zendsignaal een vierde ruimtehoekbereik (29) uitgaande van de vierde registratiepositie wordt bepaald, en waarbij het positiebereik (32) tot het vierde ruimtehoekbereik wordt beperkt.Method according to any one of the preceding claims, wherein a further sensor drone (10), to which a third RF sensor is arranged, is controlled to fly to a fourth registration position, wherein a transmission signal from the foreign drone or from the transmitter with the third RF sensor is determined, wherein a fourth solid angle range (29) starting from the fourth registration position is determined based on the determined transmission signal, and wherein the position range (32) is limited to the fourth solid angle range. 10. Sensordrone (10), waaraan een HF-sensor is aangebracht, waarbij de sensordrone ervoor is ingericht om middels de HF-sensor een HF -signaal te registreren en een ruimtehoekbereik (24, 26, 28, 29), waarin een zender van het HF -signaal van de HF-sensor uit gezien zich bevindt, te bepalen, en/of ervoor is ingericht om in het HF-signaal aanwezige identificatie- informaties en/of eigenschappen van het HF-signaal te evalueren en optioneel daarmee rekening te houden bij de bepaling van het ruimtehoekbereik, en/of ervoor is ingericht om een positiebereik van het HF- signaal in afhankelijkheid van het door de HF-sensor vastgestelde HF- signaal te bepalen.10. Sensor drone (10), to which an RF sensor is mounted, the sensor drone being designed to register an RF signal by means of the RF sensor and to determine a solid angle range (24, 26, 28, 29) in which a transmitter of the RF signal is located as seen from the RF sensor, and/or being designed to evaluate identification information and/or properties of the RF signal present in the RF signal and optionally take this into account when determining the solid angle range, and/or being designed to determine a position range of the RF signal in dependence on the RF signal detected by the RF sensor. 11. Systeem omvattende een sensordrone (10) volgens conclusie 10 en een dronestuureenheid voor de sensordrone, waarbij het systeem ervoor is ingericht om de werkwijze volgens een der conclusies 1 tot en met 9 door te voeren.A system comprising a sensor drone (10) according to claim 10 and a drone control unit for the sensor drone, the system being adapted to carry out the method according to any one of claims 1 to 9. 12. Systeem volgens conclusie 11, waarbij de dronestuureenheid een automatische stuureenheid en/of een afstandsstuureenheid voor handmatige vlucht insluit.12. A system as claimed in claim 11, wherein the drone control unit comprises an automatic control unit and/or a remote control unit for manual flight. 13. Systeem volgens conclusie 11 of 12, voorts omvattende een droneregistratiesysteem (12), dat ervoor is ingericht om een vreemde drone te registreren, een aanwezigheidsbereik van de vreemde drone (20) te bepalen, en het indringen van de vreemde drone in een gedefinieerd luchtbereik (2) te herkennen.A system according to claim 11 or 12, further comprising a drone registration system (12) adapted to register a foreign drone, determine a presence range of the foreign drone (20), and recognize the intrusion of the foreign drone into a defined air range (2).
NL2036436A 2022-12-07 2023-12-06 Method for determining a position range of a third-party drone or a transmitter of a control device of the third-party drone NL2036436B1 (en)

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