Standoff detection of motion and concealed unexploded ordnance (UXO)

• US 8,573,529 B2
• Filed: 03/01/2011
• Issued: 11/05/2013
• Est. Priority Date: 03/01/2010
• Status: Active Grant

• Current Assignee: Farrokh Mohamadi
• Original Assignee: Farrokh Mohamadi
• Inventors: Mohamadi, Farrokh
• Primary Examiner(s): Ellis, Christopher P
• Assistant Examiner(s): Badawi, Medhat
• Application Number:
  US13/037,804
• Publication Number:
  US 20110210883A1
• Time in Patent Office: 980 Days
• Field of Search: 244/23.C, 244/23.A, 244 121- 126
• US Class Current: 244/23.A
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64U 10/13 Flying platforms
• CPC Class Codes: B64U 2101/30 for imaging, photography or videography
• CPC Class Codes: B64U 30/20 Rotors; Rotor supports
• CPC Class Codes: F41H 11/136 Magnetic, electromagnetic, acoustic or radiation systems, e.g. ground penetrating radars or metal-detectors
• CPC Class Codes: F42B 12/365 Projectiles transmitting information to a remote location using optical or electronic means F42B12/385 takes precedence
• CPC Class Codes: F42B 15/08 for carrying measuring instruments; Arrangements for mounting sensitive cargo within a projectileadaptations for meteorology G01W1/08; Arrangements for acoustic sensitive cargo within a projectile
• CPC Class Codes: G01S 13/0209 Systems with very large relative bandwidth, i.e. larger than 10 %, e.g. baseband, pulse, carrier-free, ultrawideband
• CPC Class Codes: G01S 13/867 Combination of radar systems with cameras
• CPC Class Codes: G01S 13/887 for detection of concealed objects, e.g. contraband or weapons

Abstract

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 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 ultra-wideband (UWB) radar imaging system to the remote location. A method includes: remotely controlling flight of the aircraft using a main propeller and a plurality of wing unit propellers with airflow from the main propeller to the wing unit propellers for lift and propulsion; operating an ultra-wideband (UWB) radar imaging system from the aircraft; and transmitting information from the UWB radar imaging system to a display at a location remote from the aircraft.

Claims

1. A system comprising:

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 ultra-wideband (UWB) radar imaging system housed in the housing;

a control system, housed in the housing, for controlling flight of the multi-propeller aircraft from a remote location; and

a telemetry system, housed in the housing, for providing information from the ultra-wideband (UWB) radar imaging system to the remote location.

2. The system of claim 1, wherein:

the main propeller is disposed to provide a stabilizing airflow to the wing unit propellers.

3. The system of claim 1, wherein:

the housing is configured about the main propeller and wing unit propellers so as to provide a portion of the main propeller airflow to the wing unit propellers.

4. The system of claim 1, wherein the housing includes:

an outer shell;

hollow tubes that provide openings in the outer shell configured to direct airflow around and through the outer shell so that the outer shell is effectively porous with regard to cross winds.

5. The system of claim 1, wherein flight control is provided by adjusting the relative speeds of the main propeller and wing unit propellers.

6. The system of claim 1, further comprising:

video camera and global positioning system (GPS) sensors integrated with the UWB radar sensor imaging for providing real-time feedback of information.

7. 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.

8. A method comprising:

remotely controlling flight of an aircraft using a main propeller and a plurality of wing unit propellers for lift and propulsion;

operating an ultra-wideband (UWB) radar imaging system from the aircraft; and

transmitting information from the UWB radar imaging system to a display at a location remote from the aircraft.

9. The method of claim 8, wherein the step of remotely controlling flight further comprises providing a stabilizing airflow from the main propeller to the wing unit propellers.

10. The method of claim 8, further comprising:

scanning, from the aircraft, a general area of interest using the UWB radar imaging system;

performing signal analysis using data provided by the UWB radar imaging system to isolate a target of interest from clutter;

imaging the target of interest on the display at the location remote from the aircraft.

11. The method of claim 8, further comprising:

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;

imaging 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; and

imaging the results of the fine analysis on the display at the location remote from the aircraft.

12. The method of claim 8, further comprising:

stabilizing the aircraft with a flow of air directed from the main propeller to the wing unit propellers using the housing.

13. The method of claim 8, further comprising:

reducing an impact of airflow on the outside of the aircraft by directing the airflow through hollow tubes that open to an outside of an outer shell of the aircraft.

14. The method of claim 8, further comprising:

controlling flight of the aircraft by adjusting the relative speeds of the main propeller and wing unit propellers.