Patents by Inventor Rodney RODRIGUEZ ROBLES

Rodney RODRIGUEZ ROBLES has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Publication number: 20220297849
    Abstract: A method in the field of flight control laws (CLAWs) used to control a flexible structure, for example an air to air refueling flying boom system, the method detecting the physical status determined by exogenous boundary conditions acting on the flexible structure. A computer program is provided which carries out the method for detecting the physical status of a flexible structure. A system and aircraft comprising such a flexible structure are also provided.
    Type: Application
    Filed: March 15, 2022
    Publication date: September 22, 2022
    Inventors: Rodney RODRIGUEZ ROBLES, Pablo PINGARRÓN ZAPARDIEL, Francisco José ASENSIO NIETO
  • Patent number: 10514318
    Abstract: A method of aeroservoelastic coupling suppression, and particularly, the field of real time adaptive cancellation of elastic modes in discrete-time signals which measure the dynamics of a flexible structure. The flexible structure comprises a structure with elastic variable characteristics, and more particularly, a structure with non-linear aerodynamics. A method is disclosed for adaptively cancelling, in real time, N elastic modes in discrete-time signals which measure the dynamics of the flexible structure. Also disclosed is a computer program implemented on a computing device, a system and an aircraft implementing the mentioned method.
    Type: Grant
    Filed: September 25, 2017
    Date of Patent: December 24, 2019
    Assignee: AIRBUS DEFENCE AND SPACE SAU
    Inventors: Francisco José Asensio Nieto, Rodney Rodriguez Robles, Alberto Sanz De Blas
  • Publication number: 20180088000
    Abstract: A method of aeroservoelastic coupling suppression, and particularly, the field of real time adaptive cancellation of elastic modes in discrete-time signals which measure the dynamics of a flexible structure. The flexible structure comprises a structure with elastic variable characteristics, and more particularly, a structure with non-linear aerodynamics. A method is disclosed for adaptively cancelling, in real time, N elastic modes in discrete-time signals which measure the dynamics of the flexible structure. Also disclosed is a computer program implemented on a computing device, a system and an aircraft implementing the mentioned method.
    Type: Application
    Filed: September 25, 2017
    Publication date: March 29, 2018
    Inventors: Francisco José ASENSIO NIETO, Rodney RODRIGUEZ ROBLES, Alberto SANZ DE BLAS