Thruster based locomotion for perched unmanned aerial vehicles

Abstract

A system for landing and locomoting on a surface of a structure comprises an unmanned aerial vehicle having a plurality of independently controllable thrusters and an undercarriage including a frame with wheels at corners. The undercarriage further includes a plurality of bars pivotally coupled at respective first ends to the frame and coupled at respective second ends to the unmanned aerial vehicle; wherein the unmanned aerial vehicle is operative to differentially activate the plurality of thrusters so as to tilt with respect to the frame of the undercarriage and to cause a net resultant force on the undercarriage to locomote on the surface of the structure.

1 . A system for landing and locomoting on a surface of a structure comprising:
 an unmanned aerial vehicle having a plurality of independently controllable thrusters; and   an undercarriage including a frame having a plurality of corners, a set of wheels with each wheel coupled to a respective corner of the frame, and a plurality of bars pivotally coupled at respective first ends to the frame and coupled at respective second ends to the unmanned aerial vehicle,   wherein the unmanned aerial vehicle is operative to differentially activate the plurality of thrusters so as to tilt with respect to the frame of the undercarriage and to exert a net resultant force that causes the undercarriage to locomote on the surface of the structure.   
     
     
         2 . The system of  claim 1 , wherein the plurality of bars includes four bars configured in an X-shaped arrangement. 
     
     
         3 . The system of  claim 1 , wherein the unmanned aerial vehicle includes a processor configured with program code for controlling kinetic behavior of the unmanned aerial vehicle according to a flight mode, a locomotion mode, and a perch mode. 
     
     
         4 . The system of  claim 3 , wherein the set of wheels includes four wheels and the undercarriage includes pressure sensors operative to indicate a force of contact between the set of wheels and the surface of the structure. 
     
     
         5 . The system of  claim 3 , wherein the unmanned aerial vehicle includes an optical sensor and the processor is configured with program code for image processing and identification. 
     
     
         6 - 8 . (canceled) 
     
     
         9 . The system of  claim 1 , wherein at least one of the undercarriage and the unmanned aerial vehicle includes equipment for inspecting the surface of the structure. 
     
     
         10 . The system of  claim 1 , wherein the wheels of the undercarriage are one of omni-wheels and mecanum wheels. 
     
     
         11 . A method of landing and locomoting on a surface of a structure using an unmanned aerial vehicle having controllable thrusters, the method comprising:
 coupling an undercarriage including a frame having a plurality of corners, a set of wheels with each wheel coupled to a respective corner of the frame and a plurality of pivotable bars pivotally coupled at respective first ends to the frame and coupled at respective second ends to the unmanned aerial vehicle to the unmanned aerial vehicle; and   controlling the thrusters of the unmanned aerial vehicle so as to tilt the pivotable bars of the undercarriage with respect to the frame and exert a resultant force on the undercarriage that causes the undercarriage to locomote on the surface of the structure.   
     
     
         12 . The method of  claim 11 , wherein the unmanned aerial vehicle includes a plurality of thrusters and the controlling of the thrusters includes differentially activating the plurality of thrusters to obtain a net resultant force. 
     
     
         13 . The method of claim  411 , wherein the plurality of pivotable bars of the undercarriage includes four bars configured in an X-shaped arrangement. 
     
     
         14 . The method of  claim 11 , further comprising determining a kinetic mode for the unmanned vehicle consisting of one of a flight mode, a locomotion mode, and a perch mode. 
     
     
         15 . The method of  claim 14 , further comprising detecting a pressure on the set of wheels of the undercarriage indicative of a force of contact between the set of wheels and the surface of the structure. 
     
     
         16 . The method of  claim 14 , further comprising optically detecting a surface of the structure and determining a location of the unmanned aerial vehicle with respect to the surface of the structure based on the optical detection. 
     
     
         17 - 19 . (canceled) 
     
     
         20 . The method of  claim 11 , further comprising inspecting the surface of the structure. 
     
     
         21 . The method of  claim 11 , further comprising fixing the pivotable bars at a specific angle with respect to the undercarriage. 
     
     
         22 . The system of  claim 1 , wherein each of the first ends of the pivotable bars pivots about an axis which is coincident with the axle of a respective wheel. 
     
     
         23 . The system of  claim 1 , wherein each pivotable bar is rigid. 
     
     
         24 . The method of  claim 11 , wherein each of the first ends of the pivotable bars pivots about an axis which is coincident with the axle of a respective wheel. 
     
     
         25 . The method of  claim 11 , wherein each pivotable bar is rigid.