EP1952366A1 - Device for monitoring a sensitive object such as an aircraft and method for operating this device - Google Patents
Device for monitoring a sensitive object such as an aircraft and method for operating this deviceInfo
- Publication number
- EP1952366A1 EP1952366A1 EP06842002A EP06842002A EP1952366A1 EP 1952366 A1 EP1952366 A1 EP 1952366A1 EP 06842002 A EP06842002 A EP 06842002A EP 06842002 A EP06842002 A EP 06842002A EP 1952366 A1 EP1952366 A1 EP 1952366A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- monitoring
- aircraft
- images
- communication
- monitoring device
- Prior art date
- Legal status (The legal status 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 status listed.)
- Granted
Links
Classifications
-
- G—PHYSICS
- G08—SIGNALLING
- G08B—SIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
- G08B13/00—Burglar, theft or intruder alarms
- G08B13/22—Electrical actuation
- G08B13/24—Electrical actuation by interference with electromagnetic field distribution
- G08B13/2491—Intrusion detection systems, i.e. where the body of an intruder causes the interference with the electromagnetic field
- G08B13/2494—Intrusion detection systems, i.e. where the body of an intruder causes the interference with the electromagnetic field by interference with electro-magnetic field distribution combined with other electrical sensor means, e.g. microwave detectors combined with other sensor means
-
- G—PHYSICS
- G08—SIGNALLING
- G08B—SIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
- G08B13/00—Burglar, theft or intruder alarms
- G08B13/18—Actuation by interference with heat, light, or radiation of shorter wavelength; Actuation by intruding sources of heat, light, or radiation of shorter wavelength
- G08B13/189—Actuation by interference with heat, light, or radiation of shorter wavelength; Actuation by intruding sources of heat, light, or radiation of shorter wavelength using passive radiation detection systems
- G08B13/194—Actuation by interference with heat, light, or radiation of shorter wavelength; Actuation by intruding sources of heat, light, or radiation of shorter wavelength using passive radiation detection systems using image scanning and comparing systems
- G08B13/196—Actuation by interference with heat, light, or radiation of shorter wavelength; Actuation by intruding sources of heat, light, or radiation of shorter wavelength using passive radiation detection systems using image scanning and comparing systems using television cameras
- G08B13/19639—Details of the system layout
- G08B13/19647—Systems specially adapted for intrusion detection in or around a vehicle
- G08B13/1965—Systems specially adapted for intrusion detection in or around a vehicle the vehicle being an aircraft
-
- G—PHYSICS
- G08—SIGNALLING
- G08B—SIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
- G08B13/00—Burglar, theft or intruder alarms
- G08B13/18—Actuation by interference with heat, light, or radiation of shorter wavelength; Actuation by intruding sources of heat, light, or radiation of shorter wavelength
- G08B13/189—Actuation by interference with heat, light, or radiation of shorter wavelength; Actuation by intruding sources of heat, light, or radiation of shorter wavelength using passive radiation detection systems
- G08B13/194—Actuation by interference with heat, light, or radiation of shorter wavelength; Actuation by intruding sources of heat, light, or radiation of shorter wavelength using passive radiation detection systems using image scanning and comparing systems
- G08B13/196—Actuation by interference with heat, light, or radiation of shorter wavelength; Actuation by intruding sources of heat, light, or radiation of shorter wavelength using passive radiation detection systems using image scanning and comparing systems using television cameras
- G08B13/19697—Arrangements wherein non-video detectors generate an alarm themselves
-
- G—PHYSICS
- G08—SIGNALLING
- G08B—SIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
- G08B29/00—Checking or monitoring of signalling or alarm systems; Prevention or correction of operating errors, e.g. preventing unauthorised operation
- G08B29/18—Prevention or correction of operating errors
- G08B29/183—Single detectors using dual technologies
Definitions
- the present invention relates to a device for monitoring a sensitive object such as an aircraft, more particularly a business jet.
- the invention also covers the method of driving this device.
- Vandalism manifests itself in a variety of ways, for example: theft of kerosene, mechanical damage, theft of coins, or the affixing of tags.
- the solution sought is obviously an autonomous solution that avoids the permanent maintenance of a human presence and aims a remote monitoring application.
- Another object of the invention is to transmit these images by means of a telephone network to a portable device such as a mobile phone, which is available to the owner or the person of confidence in charge in particular of surveillance.
- Good consumption management also comes into play and forces us to choose the least energy-efficient solution possible.
- the application requires that the covered field be 360 °, not with a sector and a sweeping rotationally but 360 ° simultaneously so as to prevent intrusions from several directions at the same time.
- the distance of detection and capture of images it is necessary to provide a circular zone with a radius up to 50 meters around the plane to give an order of ideas. Since a camera field with an acceptable distortion at such a distance covers a maximum angle of 100 °, four cameras are needed, which also leads to a multiplication of the unit power consumption and thus to the loss of autonomy.
- a monitoring device is preferably located under the fuselage so as to cover the ground, at man's height substantially, including the landing gear which remains a very sensitive part, strongly exposed when the aircraft is on the ground, allowing also access to certain parts of the fuselage.
- Such a device being reported under the fuselage of the aircraft it must be taken into account that it must be in the central position, often to the right of the tanks hence the need to provide a separation in case of a crash. Nevertheless, the housing must be able to withstand extreme temperatures, high temperature differences, frost and abrasion.
- Such a device also poses significant problems on the detection itself since it is it which ensures the first stage of the surveillance. It is therefore necessary to achieve a high reliability of tripping with on the one hand a sensibility ensuring the detection for each real intrusion but which, on the other hand, avoids the nuisance alarms.
- the detectors themselves require a particular and sophisticated radiation guiding and convergence infrastructure to enable the sensor to work in satisfactory conditions.
- the sensors must be protected against mechanical aggression and against abrasion.
- These protections usually glasses, must be transparent to infrared radiation. But then it is necessary to combine antinomic characteristics.
- materials that are transparent to infrared radiation have low mechanical strengths and / or low resistance to large temperature variations.
- the present invention proposes a device to overcome the problems that have just been exposed, particularly applicable to aircraft, which can be implemented on new aircraft during assembly but also on aircraft in service, so a posteriori .
- FIG. 1 a schematic view of an aircraft with the positioning of the device according to the present invention
- FIG. 2 a schematic view of the device seen in side elevation
- the device according to the invention comprises a casing 10 intended to be attached to the fuselage of an aircraft as shown in FIG. 1, this casing being also the support structure of the various members constituting the elements of the aircraft. detection and visualization of said monitoring device.
- This casing is advantageously under the fuselage, partly median.
- the casing is substantially at man's height for a business jet even for the larger models.
- the housing as shown in Figures 2 and 3 comprises in the embodiment shown, a peripheral flange to be fixed on the periphery of a conjugate profile opening formed in said fuselage.
- Such a device comprises power supply means 12 such as a battery.
- This battery is recharged by the general power system of the aircraft, when the main or auxiliary power of the aircraft is active.
- the battery is of a capacity of a few amperes, in 28 volts as it should be in aeronautics and the aeronautical standards for its constitution.
- Such batteries are commercially available. The constraints related to these batteries lead to high performance products but representing an additional weight, growing rapidly with the capacity and it is therefore necessary to strongly limit the power of such a battery for an auxiliary system so that the monitoring system in together contributes to a lower weight increase.
- This battery is advantageously housed in the fuselage.
- a calculator 14 is provided. This calculator is intended to process the data of the system and since it does not need access on the outside of the aircraft, as will be explained below, it is also housed in the fuselage.
- the general volume of the housing 10 is itself greatly reduced, requiring a high compactness of the interior arrangement.
- this housing being a source of aerodynamic disturbances, it should be minimized since total suppression is impossible and it must necessarily protrude as will be indicated later.
- the components internal to the housing that constitute the monitoring device itself essentially comprise means 16 for detecting by microwave frequencies, means 18 for capturing images.
- the device according to the invention is not content to trigger an alarm in case of break-in but to monitor a given area corresponding to a security perimeter around the aircraft.
- the device monitors a given area including the environment of the aircraft through the detection means 16, and, in the event of detection of an intrusion into said environment, captures images of the environment of the aircraft thanks to the means 18 for capturing images.
- the microwave detection means 16 are preferably housed in the lower part of the housing 10 so that they can scan 360 ° without encountering obstacles.
- These means 16 may comprise four receiving antennas and an omnidirectional transmitting antenna or as in the present case four emitter antennas 26 and an omnidirectional receiving antenna 28.
- This choice is retained for its ability to enable management by generating lower energy consumption.
- Each transmitting antenna covers a sector slightly greater than 90 ° in order to generate a superposition and to cover certainly 360 °.
- the material constituting the casing and located at the right of these transmitting and receiving antennas is transparent to the microwave, which is not a problem and can be for example a composite material. It is therefore noted that the problems associated with abrasion, with frost, with the specific material of the windows, as in the case of infrared radiation, for example, with the capture of the radiations, are suppressed, which is a response of the present invention to the problem. posed.
- these detection means 16 are insensitive to heat, cold and do not cause inadvertent tripping related to these parameters.
- microwave detection means 16 The scope of these microwave detection means 16 is of the order of
- microwave detection means 16 trigger a signal as soon as the receiving antenna picks up at least one disturbance in its control field.
- This signal is transmitted to the control means 24.
- the image capture means 18 in the preferential embodiment retained comprise at least one camera and in this case four digital cameras 30. Each camera has a cover with an angle of about 90 °.
- These cameras are also energy-hungry and they are associated with a sequential switch 32 which makes it possible to provoke an image capture on a single camera at a time but successively, by circular permutation and at a high frequency, several times per second for give an idea.
- a sequential switch 32 which makes it possible to provoke an image capture on a single camera at a time but successively, by circular permutation and at a high frequency, several times per second for give an idea.
- each camera it is possible from each camera to have animated images, a quality, including a largely sufficient definition to see without difficulty the intrusion, while significantly reducing energy consumption.
- This driving of the camera park is transparent and imperceptible to the person in charge of reading the images.
- the means 20 for processing and storing the images acquired by each of the cameras allow compression of the digital files so as to allow storage, for example on a Secure Digital SD memory card whose access time is very fast and whose capacity is sufficient to memorize the sequences of intrusion in the field of the cameras.
- processing and storage means 20 are accessible and managed by the control means 24 integrated in the computer.
- Transmission means 22 comprise a transmitter / receiver 34 of the same type as in the field of wireless telephony and capable of operating on the wireless telephone network.
- These transmission means allow the sending of files and the sending and receiving of instructions 24 means of control from a mobile phone on a wireless telephone network and / or through a communication network close by a private wireless connection like the one called "Bluetooth" for example.
- the operator can perform many interventions such as:
- proximity "Bluetooth” type an additional communication called proximity "Bluetooth” type. Indeed, in case of non coverage by the mobile network, in case of total failure, in case of temporary break of the link or simply to operate in local mode near the device, on interrogation of the system, the operator is informed upon arrival in the proximity coverage area of an alert on his / her mobile.
- the owner or any person in charge of the surveillance of the airplane leaves the aircraft, it activates the monitoring device voluntarily or the system warns after a certain period that the device is not in service.
- the microwave detection means 16 are in use and the emitter antennas scan their sectors, the receiving antenna ensuring the detection of a disturbance of the monitored field, especially during an intrusion.
- control means trigger an alarm and a transmission of a signal to the owner or the person responsible for monitoring the aircraft.
- This signal is advantageously an SMS (Short Message Service).
- SMS Short Message Service
- the cameras are put into service, preferably sequentially, as indicated above, the acquired images being processed in particular compressed and stored.
- the owner or the person responsible for surveillance can then consult with very slight deferred images acquired and take the necessary measures in case of discovery of an intrusion.
- the cover captures images 360 ° so provide all the information even if there are several people from different directions.
- the operator wants to see the immediate environment of the aircraft, for example the possible presence of a plane parked nearby, he can visualize with each camera the field concerned.
- the range of the camera is much greater than that of triggering the detection means, thanks to a large depth of field.
- the means of detection must be limited to the enlarged perimeter of the airplane so that they are not disturbed by the regular and normal movements of the aircraft. personnel and equipment on the ground that would trigger irrelevant alarms.
- the monitoring device in its fixed housing version, is completed by a so-called CA approval camera.
- This camera is housed in the housing 10 and it is located on the front with a tilt angle so as to acquire images of the ground especially during the take-off and landing phases.
- the camera is a color camera and the images are transmitted on monitors in passenger seats for the pleasure of the flight, these images complementing in an attractive and inf ormative way the vision through the portholes.
- the microwave detection means 16 are preferably housed in the lower part of the housing 10 so that they can be swept away.
- these means 16 could be positioned in a first independent housing and connected to the computer while the surveillance cameras would be housed in a second housing also connected to the computer.
- crankcase This separation of functions and constituents may be of interest in the case where the projection has to be reduced. Indeed, the number of crankcase is multiplied by two but the aerodynamic disturbances generated by these two crankcases of smaller dimensions can be lower than that of a crankcase. only larger casing. Nevertheless, there remains the need for two integrations in the fuselage.
- These means 16 advantageously comprise four transmitting antennas
- the housing is connected to the bodies located in the fuselage namely battery and computer by a suitable wiring provided with at least one connection so as to easily remove the housing and its contents before the flight and to be able to re install a once the aircraft is parked and parked.
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Electromagnetism (AREA)
- Computer Security & Cryptography (AREA)
- Aviation & Aerospace Engineering (AREA)
- Multimedia (AREA)
- Closed-Circuit Television Systems (AREA)
- Alarm Systems (AREA)
- Studio Devices (AREA)
- Burglar Alarm Systems (AREA)
- Radar Systems Or Details Thereof (AREA)
- Mobile Radio Communication Systems (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0553363A FR2893169A1 (en) | 2005-11-07 | 2005-11-07 | DEVICE FOR MONITORING A SENSITIVE OBJECT SUCH AS AN AIRCRAFT AND METHOD OF CONDUCTING IT |
PCT/FR2006/051141 WO2007051955A1 (en) | 2005-11-07 | 2006-11-06 | Device for monitoring a sensitive object such as an aircraft and method for operating this device |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1952366A1 true EP1952366A1 (en) | 2008-08-06 |
EP1952366B1 EP1952366B1 (en) | 2010-01-13 |
Family
ID=36698624
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP06842002A Not-in-force EP1952366B1 (en) | 2005-11-07 | 2006-11-06 | Device and method for monitoring a sensitive object such as an aircraft |
Country Status (5)
Country | Link |
---|---|
EP (1) | EP1952366B1 (en) |
AT (1) | ATE455341T1 (en) |
DE (1) | DE602006011779D1 (en) |
FR (1) | FR2893169A1 (en) |
WO (1) | WO2007051955A1 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2911987B1 (en) * | 2007-01-29 | 2010-08-13 | Airbus France | METHOD OF MONITORING AUTHORIZED AND UNAUTHORIZED PERSONS IN A SECURITY PERIMETER AROUND A DEVICE |
FR2915303B1 (en) * | 2007-04-23 | 2011-04-29 | Airbus France | DEVICE AND METHOD FOR PROTECTION AGAINST INTRUSIONS IN AIR TRAIN HOUSING |
FR3020704B1 (en) * | 2014-05-02 | 2016-05-27 | Airbus | PREVENTING RISKS DURING INTERVENTION ON AN AIRCRAFT |
CN107990939A (en) * | 2017-12-04 | 2018-05-04 | 北京理工大学 | A kind of multipurpose real-time monitoring system for complex environment based on Internet of Things |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2250156B (en) * | 1990-10-06 | 1994-04-06 | Chubb Electronics Ltd | Video surveillance system |
US5319350A (en) * | 1992-12-29 | 1994-06-07 | Demarco Frank | Motion detection assembly for use in combination with a motor vehicle |
US5917405A (en) * | 1993-06-08 | 1999-06-29 | Joao; Raymond Anthony | Control apparatus and methods for vehicles |
US20020171557A1 (en) * | 2001-05-18 | 2002-11-21 | Wegener William E. | Security electronic system |
DE20112085U1 (en) * | 2001-07-20 | 2002-04-04 | Schmiedt Ralf | System for the observation and filming of vehicles, people and objects from the air |
FR2851108A1 (en) * | 2003-02-06 | 2004-08-13 | Michel Maurice Eeckman | Burglary offences recording and processing device for shop and public building, has digital camera associated with GPS to capture images, which are transmitted in radio or wireless manner to computer of security professionals |
-
2005
- 2005-11-07 FR FR0553363A patent/FR2893169A1/en not_active Withdrawn
-
2006
- 2006-11-06 WO PCT/FR2006/051141 patent/WO2007051955A1/en active Application Filing
- 2006-11-06 DE DE602006011779T patent/DE602006011779D1/en active Active
- 2006-11-06 AT AT06842002T patent/ATE455341T1/en not_active IP Right Cessation
- 2006-11-06 EP EP06842002A patent/EP1952366B1/en not_active Not-in-force
Non-Patent Citations (1)
Title |
---|
See references of WO2007051955A1 * |
Also Published As
Publication number | Publication date |
---|---|
ATE455341T1 (en) | 2010-01-15 |
DE602006011779D1 (en) | 2010-03-04 |
EP1952366B1 (en) | 2010-01-13 |
FR2893169A1 (en) | 2007-05-11 |
WO2007051955A1 (en) | 2007-05-10 |
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