초록 ▼

A surveillance system includes a multi-propeller aircraft having a main propeller and a plurality of wing unit propellers; a housing that houses the main propeller and the wing unit propellers; an optical video camera; an ultra-wideband (UWB) radar imaging system; a control system for controlling fl

A surveillance system includes a multi-propeller aircraft having a main propeller and a plurality of wing unit propellers; a housing that houses the main propeller and the wing unit propellers; an optical video camera; an ultra-wideband (UWB) radar imaging system; a control system for controlling flight of the multi-propeller aircraft from a remote location; and a telemetry system for providing information from the optical camera and the ultra-wideband (UWB) radar imaging system to a remote location.

대표청구항 ▼

1. A system comprising: a multi-propeller aircraft having a plurality of wing unit propellers for vertical takeoff and landing;a housing that houses a main propeller and the wing unit propellers, the housing having a diameter of approximately 1.5 feet to 3 feet;an ultra-wideband (UWB) radar imaging

1. A system comprising: a multi-propeller aircraft having a plurality of wing unit propellers for vertical takeoff and landing;a housing that houses a main propeller and the wing unit propellers, the housing having a diameter of approximately 1.5 feet to 3 feet;an ultra-wideband (UWB) radar imaging system housed in the housing;an optical camera within the housing:a control system, housed in the housing, for controlling flight of the multi-propeller aircraft from a remote location;a microwave transmitter configured to heat water within or on one or more ground surfaces;an infrared camera for detecting a heat signature of a ground surface in response to the heating from the microwave transmitter; anda telemetry system, housed in the housing, for providing information from the ultra-wideband (UWB) radar imaging system and the optical camera to the remote location, wherein the system is configured to first interrogate a ground surface with the optical camera to locate disturbed ground surfaces and with the microwave transmitter and the infrared camera to locate a disturbed ground surface by detecting a thermal profile of the disturbed ground in response to the heating from the microwave transmitter based on the disturbed ground having a different dewpoint and thus a correspondingly different thermal profile from undisturbed ground andto subsequently interrogate the disturbed ground surface with the UWB radar imaging system, wherein the system is further configured to:scan, from the aircraft, a general area of interest using a first UWB radar system operating at a first center frequency;perform a coarse analysis using data provided by the first radar system to isolate a target of interest from clutter;display imaging of the target of interest on a display at the remote location;remotely direct the aircraft to scan the target of interest using a second ultra-wideband (UWB) radar system operating at a second center frequency that is higher than the first center frequency;perform a fine analysis using narrow beam data provided by the second radar system; anddisplay imaging of the results of the fine analysis on the display at the remote location. 2. The system of clam 1, wherein the multi-propeller aircraft further includes an explosive discoloration agent spray system to spray the interrogated disturbed ground surface with explosive discoloration agent to authenticate the presence of buried IEDs. 3. The system of claim 1, further comprising: a global positioning system (GPS) sensor integrated with the UWB radar sensor imaging for providing real-time feedback of information. 4. The system of claim 1, wherein: real-time feedback of information from the ultra-wideband (UWB) radar imaging system is available on a display for remote control operation of the aircraft. 5. A method comprising: remotely controlling flight of an aircraft using a plurality of wing unit propellers for vertical take off and landing;operating an optical video camera mounted on the aircraft to detect the presence of disturbed ground patches;operating a microwave transmitter configured to heat water within or on one or more ground patches;operating an infrared camera for detecting a heat signature of at least one of the ground patches in response to the heating from the microwave transmitter to locate a disturbed ground patch having a different dewpoint and thus a correspondingly different thermal profile from undisturbed ground in response to the heating from the microwave transmitter;operating an ultra-wideband (UWB) radar imaging system from the aircraft to image the disturbed ground patches for the presence of buried improvised explosive devices (IEDs) from a height of approximately 1 to 5feet from the disturbed ground patches;scanning, from the aircraft, a general area of interest using a first UWB radar system operating at a first center frequency;performing a coarse analysis using data provided by the first radar system to isolate a target of interest from clutter;transmitting information from the UWB radar imaging system to a display at a location remote from the aircraft;displaying imaging of the target of interest on the display at the location remote from the aircraft;remotely directing the aircraft to scan the target using a second ultra-wideband (UWB) radar system operating at a second center frequency that is higher than the first center frequency;performing a fine analysis using narrow beam data provided by the second radar system; anddisplaying imaging of the results of the fine analysis on the display at the location remote from the aircraft. 6. The method of claim 5, further comprising: spraying an explosive discoloration agent, that reacts with common explosive materials, on the interrogated disturbed ground surface to authenticate the presence of buried IEDs. 7. A method comprising: remotely controlling flight of an aircraft using a plurality of wing unit propellers for vertical take off and landing;operating an optical video camera mounted on the aircraft to detect the presence of disturbed ground patches;operating an ultra-wideband (UWB) radar imaging system from the aircraft to image the disturbed ground patches for the presence of buried improvised explosive devices (IEDs) from a height of approximately 1to 5feet from the disturbed ground patches;transmitting information from the UWB radar imaging system to a display at a location remote from the aircraft;from the aircraft, exciting a disturbed surface of at least one of the disturbed ground patches with a microwave transmitter configured to heat water within the disturbed surface, wherein the optical video camera comprises an infrared camera configured to detect a heat signature of the excited disturbed surface having a different dewpoint and thus a correspondingly different heat signature from undisturbed ground in response to the heating from the microwave transmitter;scanning, from the aircraft, a general area of interest using a first UWB radar system operating at a first center frequency;performing a coarse analysis using data provided by the first radar system to isolate a target of interest from clutter;displaying imaging of the target of interest on the display at the location remote from the aircraft;remotely directing the aircraft to scan the target using a second ultra-wideband (UWB) radar system operating at a second center frequency that is higher than the first center frequency;performing a fine analysis using narrow beam data provided by the second radar system; anddisplaying imaging of the results of the fine analysis on the display at the location remote from the aircraft. 8. The method of claim 7, wherein operating the optical video camera comprises performing an image processing texture filtering. 9. The method of claim 7, further comprising: marking the imaged target of interest by spraying one of the disturbed ground patches with an explosive discoloration agent.