COMPUTER HARDWARE LAUNCH

Brand Owner (click to sort) Address Description
INSIGHT Insitu, Inc. 118 East Columbia River Way Bingen WA 98605 Computer hardware for launch, operation, and retrieval of unmanned aerial vehicles; computer software for control of remote ground control systems used in launching, operating, and retrieving unmanned aerial vehicles, and for airborne control of unmanned aerial vehicles; aircraft, airplane and unmanned aerial vehicle components and ground control components, namely, computer software for controlling remote controls for unmanned vehicles;
MAKING IDEAS SOAR Insitu, Inc. 118 East Columbia River Way Bingen WA 98605 Computer hardware for launch, operation, and retrieval of unmanned aerial vehicles; Computer hardware, namely, data processors, satellite signal processors, signal processors, video processors, mobile data receivers and radar receivers; Computer software for gathering, analyzing, transmitting, maintaining and organizing data and images for intelligence, surveillance and reconnaissance purposes, for control of remote ground control systems used in launching, operating, and retrieving unmanned aerial vehicles, and for airborne control of unmanned aerial vehicles; Unmanned aerial vehicle (UAV) components, namely, acceleration sensors, ultrasonic sensors, timing sensors, proximity sensors, temperature sensors, vehicle mounted GPS sensors for determining the rate of motion for a vehicle, motion sensors, pollutant sensors, biological sensors, chemical sensors, nuclear contamination sensors, pressure sensors, inertial navigation sensors and avionic sensor systems, namely, aircraft airspeed, altitude, and attitude sensors; Aircraft, airplane and unmanned aerial vehicle (UAV) components and ground control components, namely, remote ground control terminals comprised of manipulators for remote operation of unmanned aerial vehicles (UAVs) and cameras, remote ground controls for unmanned aerial vehicles (UAVs) and cameras, computer hardware for remote ground control of unmanned aerial vehicles (UAVs) and cameras; Radio, electronic, electro-magnetic, satellite, infrared, fiber-optic and optical data links comprised of ground control systems and airborne data systems that allow the unmanned aerial vehicle to be controlled by the ground operators and further allow data to be transmitted from the unmanned aerial vehicle to the ground operators; Ground control systems for use with unmanned aerial vehicles consisting of computer hardware and LAN, VPN and WAN operating software, video monitors, antennas, display processors, namely processors to enhance, clarify, magnify, manipulate, store and transmit displays of images, data, videos, graphics, and photographs, and video receivers; Computer software for controlling remote controls for unmanned aerial vehicles; Flight simulators for training in the use of UAVs to simulate unmanned aerial vehicle flight; Computer software featuring programs used for interactive training courseware in the field of use of unmanned aerial vehicles; Video tapes featuring training in and utilization of unmanned aerial vehicles; Airborne surveillance and aircraft control apparatus, namely, radars, low light cameras, thermal imaging cameras, GPS satellite receivers, radio altimeters, inertial navigation systems for vehicles and ground proximity sensors; Reconnaissance and surveillance apparatus, namely, electric and electronic video, audio, and data surveillance installations;
 

Where the owner name is not linked, that owner no longer owns the brand

    
Technical Examples
  1. Methods and apparatuses for launching unmanned aircraft and other flight devices or projectiles are described. In one embodiment, the aircraft can be launched from an apparatus that includes a launch carriage that moves along a launch guide. The carriage can accelerate when portions of the carriage and/or the launch guide move relative to each other. A gripper carried by the launch carriage can have at least one grip portion in contact with the aircraft while the launch carriage accelerates along the launch axis. The at least one grip portion can move out of contact with the aircraft as the launch carriage decelerates, releasing the aircraft for takeoff. A brake can arrest the motion of the gripper after launch.