Patents by Inventor Christopher A. Launer

Christopher A. Launer 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: 9945828
    Abstract: A self-contained UAV sensor payload and on-board or off-board hardware and software for precision agriculture. The invention combines multiple cameras and navigation sensors to create a system for automatically collecting, geo-referencing, and stitching red, green, blue, and near infrared imagery and derived vegetation indices. The invention is able to produce all of these quantities in a single flight. The tight integration with integrated navigation sensors eliminates the need for integration with external sensors or avionics hardware and enables innovative solutions to image processing and analysis which greatly improve accuracy, processing speed, and reliability over alternative approaches.
    Type: Grant
    Filed: October 23, 2015
    Date of Patent: April 17, 2018
    Assignee: SENTEK SYSTEMS LLC
    Inventors: Bryan T. Poling, Kimberly A. Salant, Theodore C. Poling, Christopher A. Launer
  • Patent number: 7699261
    Abstract: An unmanned aerial vehicle (UAV) is designed for low-speed, low altitude, long endurance missions typical to UAVs of this size and class. The UAV structure is configured to be substantially impervious to small arms fire and to have a very small representative radar cross-section. The UAV is modular such that the main wings and tail wing assembly are quickly and easily, detached from the fuselage for ease of transport and to provide an airframe that is quickly and easily adapted to any particular mission.
    Type: Grant
    Filed: March 5, 2007
    Date of Patent: April 20, 2010
    Assignee: Lockheed Martin Corporation
    Inventors: Todd M. Colten, Scott E. Morgan, Christopher A. Launer
  • Publication number: 20080217486
    Abstract: An unmanned aerial vehicle (UAV) is designed for low-speed, low altitude, long endurance missions typical to UAVs of this size and class. The UAV structure is configured to be substantially impervious to small arms fire and to have a very small representative radar cross-section. The UAV is modular such that the main wings and tail wing assembly are quickly and easily, detached from the fuselage for ease of transport and to provide an airframe that is quickly and easily adapted to any particular mission.
    Type: Application
    Filed: March 5, 2007
    Publication date: September 11, 2008
    Applicant: Lockheed Martin Corporation
    Inventors: Todd M. Colten, Scott E. Morgan, Christopher A. Launer