Patents by Inventor Di-Yang Wang

Di-Yang Wang 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).

  • Patent number: 11884406
    Abstract: The present application provides a system for unmanned aerial vehicle (UAV) parachute landing. An exemplary system includes a detector configured to detect at least one of a flight speed, a wind speed, a wind direction, a position, a height, and a voltage of a UAV. The system also includes a memory storing instructions and a processor configured to execute the instructions to cause the system to: determine whether to open a parachute of the UAV in accordance with a criterion, responsive to the determination to open the parachute of the UAV, stop a motor of the UAV that spins a propeller of the UAV, and open the parachute of the UAV after stopping the motor of the UAV for a first period.
    Type: Grant
    Filed: January 8, 2019
    Date of Patent: January 30, 2024
    Assignee: GEOSAT Aerospace & Technology
    Inventors: Lung-Shun Shih, Fu-Kai Yang, Yi-Feng Cheng, Di-Yang Wang, Chien-Hsun Liao
  • Publication number: 20220153404
    Abstract: The present application provides an unmanned aerial vehicle (UAV) for a long duration flight. An exemplary UAV may include a UAV body assembly. The UAV may also include a flight control system (FCS) coupled to the UAV body assembly. The UAV may further include a motor coupled to the UAV body assembly at one end and coupled to a propeller at the other end. The FCS is communicatively connected to the motor. A center of gravity (CG) of the UAV is at a point between 21% and 25% of a mean aerodynamic chord (MAC) of the UAV.
    Type: Application
    Filed: February 1, 2022
    Publication date: May 19, 2022
    Applicant: GEOSAT Aerospace & Technology
    Inventors: Fu-Kai YANG, Chien-Hsun LIAO, Yi-Feng CHENG, Di-Yang WANG, Meng-Yan SHEN
  • Patent number: 11267555
    Abstract: The present application provides an unmanned aerial vehicle (UAV) for a long duration flight. An exemplary UAV may include a UAV body assembly. The UAV may also include a flight control system (FCS) coupled to the UAV body assembly. The UAV may further include a motor coupled to the UAV body assembly at one end and coupled to a propeller at the other end. The FCS is communicatively connected to the motor. A center of gravity (CG) of the UAV is at a point between 21% and 25% of a mean aerodynamic chord (MAC) of the UAV.
    Type: Grant
    Filed: January 7, 2019
    Date of Patent: March 8, 2022
    Assignee: GEOSAT AEROSPACE & TECHNOLOGY
    Inventors: Fu-Kai Yang, Chien-Hsun Liao, Yi-Feng Cheng, Di-Yang Wang, Meng-Yan Shen
  • Publication number: 20190210735
    Abstract: The present application provides a system for unmanned aerial vehicle (UAV) parachute landing. An exemplary system includes a detector configured to detect at least one of a flight speed, a wind speed, a wind direction, a position, a height, and a voltage of a UAV. The system also includes a memory storing instructions and a processor configured to execute the instructions to cause the system to: determine whether to open a parachute of the UAV in accordance with a criterion, responsive to the determination to open the parachute of the UAV, stop a motor of the UAV that spins a propeller of the UAV, and open the parachute of the UAV after stopping the motor of the UAV for a first period.
    Type: Application
    Filed: January 8, 2019
    Publication date: July 11, 2019
    Applicant: GEOSAT Aerospace & Technology
    Inventors: Lung-Shun SHIH, Fu-Kai YANG, Yi-Feng CHENG, Di-Yang WANG, Chien-Hsun LIAO
  • Publication number: 20190210713
    Abstract: The present application provides an unmanned aerial vehicle (UAV) for a long duration flight. An exemplary UAV may include a UAV body assembly. The UAV may also include a flight control system (FCS) coupled to the UAV body assembly. The UAV may further include a motor coupled to the UAV body assembly at one end and coupled to a propeller at the other end. The FCS is communicatively connected to the motor. A center of gravity (CG) of the UAV is at a point between 21% and 25% of a mean aerodynamic chord (MAC) of the UAV.
    Type: Application
    Filed: January 7, 2019
    Publication date: July 11, 2019
    Applicant: GEOSAT Aerospace & Technology
    Inventors: Fu-Kai Yang, Chien-Hsun Liao, Yi-Feng Cheng, Di-Yang Wang, Meng-Yan Shen