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Hardware Standard Main Processor Main Processor Clock Flash Memory RAM Failsafe Co-Processor Price (USD) @ Supplier 2022/11/18 IMU / Sensors Note Autopilot 1x Veronte Embention: Propietary (user-programmable) DO178C DO254 / DO160 Texas Instruments Dual-Core NA NA NA Yes 6000 3x IMU 3x Magnetometer 2x Static 1x Pitot 2x GNSS receivers 1x Temperature
The inside of the Bayraktar TB2 GCS. GCS hardware refers to the complete set of ground-based hardware systems used to control the UAV. This typically includes the Human-Machine Interface, computer, telemetry, video capture card and aerials for the control, video and data links to the UAV.
Modern system hardware for UAV control is often called the flight controller (FC), flight controller board (FCB) or autopilot. Common UAV-systems control hardware typically incorporate a primary microprocessor, a secondary or failsafe processor, and sensors such as accelerometers, gyroscopes, magnetometers, and barometers into a single module.
An unmanned vehicle's flight controller, also referred to as an FC, FCB (flight control board), FMU (flight management unit), or autopilot, is a combination of hardware and software that is responsible for interfacing with a variety of onboard sensors and control systems in order to facilitate remote control or provide fully autonomous control.
BlueROV2 diving with ArduSub. The ArduPilot software suite consists of navigation software (typically referred to as firmware when it is compiled to binary form for microcontroller hardware targets) running on the vehicle (either Copter, Plane, Rover, AntennaTracker, or Sub), along with ground station controlling software including Mission Planner, APM Planner, QGroundControl, MavProxy, Tower ...
In order to ensure that the component architecture is applicable to the entire domain of current and future unmanned systems, it is built on five principles: vehicle platform independence, mission isolation, computer hardware independence, technology independence, and operator use independence.