Ex Parte Nelson - Page 6




               Appeal No. 2003-0622                                                                      Page 6                  
               Application No. 09/974,545                                                                                        


               activates these three devices [the rudder bar, control column, and the air brake], which                          
               are provided for this purpose with dual controls of the type found in aviation schools”                           
               (translation, page 2), and that this robotic action “transfers the possibility of                                 
               maneuvering and, thus, the control of the flight to the control tower, thereby eliminating                        
               the pilot” (translation, page 3).  Borthayre ‘842 states in his claim 1 that the method                           
               “transfers the work of the pilot to the control tower from which the plane departed, and                          
               which can now return the plane to the departing base by means of radio controls”                                  
               (translation, page 5).  Borthayre ‘842 does not disclose that the aircraft is equipped with                       
               an autopilot.  However, if the aircraft were equipped with an autopilot system, it is our                         
               view that it would be reasonable to assume from the above-cited teachings of the                                  
               reference that the control tower takes “complete and exclusive control” of the controls of                        
               the aircraft and that the autopilot also would be deactivated at least to the extent that it                      
               cannot be operated by the pilot.                                                                                  
                      The appellant’s claim 1 requires that there be a module aboard the aircraft                                
               and that “the module” (emphasis added), in response to sensing a predetermined                                    
               override input, performs the following three operations:                                                          
                      (1) Deactivates on-board control of predetermined aircraft flight systems.                                 
                      (2) Deactivates on-board control of the autopilot system.                                                  
                      (3) Directs the autopilot system to fly the aircraft to a landing.                                         









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