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Olivier Antonia Toupet

age ~44

from Escondido, CA

Also known as:
  • Olivier A Toupet
  • Oliver Antonia Toupet
  • Toupet Olivier

Olivier Toupet Phones & Addresses

  • Escondido, CA
  • Dana Point, CA
  • Santa Clarita, CA
  • Irvine, CA
  • Fremont, CA
  • Cambridge, MA
  • Los Angeles, CA

Us Patents

  • Online Optimization-Based Flight Control System

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  • US Patent:
    20200031461, Jan 30, 2020
  • Filed:
    Jun 14, 2019
  • Appl. No.:
    16/441642
  • Inventors:
    - Mountain View CA, US
    Gabe Hoffmann - Mountain View CA, US
    Olivier Toupet - Stevenson Ranch CA, US
  • International Classification:
    B64C 29/00
    G05D 1/08
    B64C 27/28
    G05D 1/10
  • Abstract:
    Techniques to control flight of an aircraft are disclosed. In various embodiments, a set of inputs associated with a requested set of forces and moments to be applied to the aircraft is received. An optimal mix of actuators and associated actuator parameters to achieve to an extent practical the requested forces and moments is determined, including by minimizing a weighted set of costs that includes costs associated with one or more errors each corresponding to a difference between a requested force or moment and a corresponding force or moment achieved by the computed solution.
  • Online Optimization-Based Flight Control System

    view source
  • US Patent:
    20190202546, Jul 4, 2019
  • Filed:
    Oct 18, 2016
  • Appl. No.:
    15/297029
  • Inventors:
    - Mountain View CA, US
    Gabe Hoffmann - Mountain View CA, US
    Olivier Toupet - Stevenson Ranch CA, US
  • International Classification:
    B64C 19/02
    B64C 27/10
    G05D 1/10
    B64C 13/18
  • Abstract:
    Techniques to control flight of an aircraft are disclosed. In various embodiments, a set of inputs associated with a requested set of forces and moments to be applied to the aircraft is received. An optimal mix of actuators and associated actuator parameters to achieve to an extent practical the requested forces and moments is determined, including by minimizing a weighted set of costs that includes costs associated with one or more errors each corresponding to a difference between a requested force or moment and a corresponding force or moment achieved by the computed solution.

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