초록 ▼

Systems and methods for protecting an airborne platform against collisions are provided. One system includes FMCW radar sensors including transmitting antennae, means for receiving signals from echoes and for processing and digitizing same, and means for sending a central unit data representing said

Systems and methods for protecting an airborne platform against collisions are provided. One system includes FMCW radar sensors including transmitting antennae, means for receiving signals from echoes and for processing and digitizing same, and means for sending a central unit data representing said digital signals via a dedicated point to point link. The central unit includes means for processing said data to detect obstacles, means for calculating parameters for each obstacle including its radial velocity, distance range and azimuth, and means to transmit an avionic system of said platform data representing said detected obstacles and parameters. The system further includes means for guaranteeing that said emitted signals are shifted in time to create a shift in frequency guaranteeing that the radar sensors operate in the whole frequency band without perturbing each other.

대표청구항 ▼

1. A protecting system for protecting an airborne platform against collisions with obstacles, said system comprising: at least one central unit;at least two identical FMCW radar sensors on the surface of said airborne platform and designed to operate in the entirety of a same frequency band, the fre

1. A protecting system for protecting an airborne platform against collisions with obstacles, said system comprising: at least one central unit;at least two identical FMCW radar sensors on the surface of said airborne platform and designed to operate in the entirety of a same frequency band, the frequency band starting at a minimum frequency and ending at a maximum frequency, each said FMCW radar sensor being connected to said central unit via a first dedicated point to point link, and comprising: at least one transmitting antenna for transmitting a FMCW signal;at least two receiving channels, each channel comprising a receiving antenna for generating a received signal from the echoes reflected by at least one of said obstacles, and means for demodulating, filtering and digitizing said received signal into a digital signal, said receiving antennae being arranged to allow measurement of at least an azimuth of said at least one obstacle; anda first interface configured to send said central unit data representing said digital signals via said first dedicated point to point link;said at least one central unit comprising: a second interface configured to receive, via each said first dedicated point to point link, said data sent by each said FMCW radar sensor;a processor configured to process said data to detect said obstacles in a field of view of said FMCW radar sensors;a calculator module configured to calculate parameters for each said detected obstacle, said parameters comprising at least a radial velocity, a distance range and an azimuth range of said obstacle; anda generator and transmitter module configured to generate and transmit to an avionic system of said airborne platform data representing said detected obstacles and their said parameters; anda synchronization module configured to shift said FMCW signals emitted by said transmitting antennae in time to create a shift in frequency such that each FMCW radar sensor generates a signal in the entirety of said frequency band, the signal starting at the minimum frequency and ending at the maximum frequency, without being perturbed by said neighboring FMCW radar sensors. 2. A protecting system according to claim 1, wherein said synchronization module comprises: a third interface of said central unit configured to simultaneously send a synchronization signal to each of said FMCW radar sensors; anda sensor delay module of said FMCW radar sensors configured to determine a delay to wait before starting transmitting said FMCW signal after reception of said synchronizing signal. 3. A protecting system according to claim 2, comprising: one central unit configured as a master central unit and at least one central unit configured as a slave central unit, each central unit being connected to corresponding FMCW radar sensors;said at least one slave central unit configured to receive said synchronization signal from said master central unit and to route said synchronization signal towards said corresponding FMCW radar sensors;each said central unit including a processing unit configured to calculate said parameters of each detected obstacles;said at least one said central unit configured to transmit said parameters towards said master central unit;said master central unit configured to merge said obstacles and to transmit the resulting data representing said obstacles and their parameters to said avionic system. 4. A protecting system according to claim 1, wherein said central unit is configured to send said synchronization signal to said FMCW radar sensors via a second point to point dedicated link different from said first dedicated point to point link, each said second point to point dedicated link being a differential line. 5. A protecting system according to claim 1, further comprising: an evaluation module configured to evaluate a dangerousness of said detected obstacles from said parameters; anda classification module configured to classify said detected obstacles according to their dangerousness. 6. A protecting system according to claim 1, wherein said first dedicated point to point link is an Ethernet full duplex link, said data being encapsulated into Ethernet frames. 7. A protecting system according to claim 1, wherein said at least one central unit further comprises a filtering module configured to filter said received signals due to echoes reflected by the envelope of said airborne platform according to at least one of said parameters of said envelope. 8. A protecting system according to claim 1, wherein said receiving antennae are arranged in said sensor unit to further allow the measurement of the elevation of said at least one obstacle, said parameters of each said detected obstacle also comprising its elevation. 9. A protecting system according to claim 1, wherein said at least one central unit further comprises a merging module configured to merge said obstacles detected by at least two said different FMCW radar sensors. 10. A protecting system according to claim 1, wherein at least one of said FMCW radar sensors further comprises a deactivation module configured to deactivate the at least one FMCW radar sensor if the temperature inside that sensor is higher than a determined threshold. 11. A protecting system according to claim 1, wherein said processor detects said obstacles based on at least one flight parameter of the airborne platform. 12. A protecting system according to claim 1, further comprising an obstruction module configured to detect that at least one of said FMCW radar sensor is obstructed. 13. A protecting system according to claim 1, wherein at least one said FMCW radar sensor is powered from said central unit. 14. A protecting system according to claim 1, wherein said central unit comprises a third interface configured to send at least one of said FMCW radar sensor a command to deactivate the transmitting radio components of said sensor. 15. A protecting system according to claim 1, wherein said antennae are patch antennae.