The AP is resilient against jamming and features precise dead-reckoning navigation in absence of a GNSS signal. In D3 (Dirty-Dull-Dangerous) UAV applications flight conditions may vary on large. The flight control algorithm relies on Total Energy Control System (TECS) for improved reliability and response to malfunction including automatic landing with engine failure, auto-rotation for helicopters and parachute deployment. Unmanned aerial vehicles are famous for their wide range of applications. The ailerons, elevator (or stabilator), and rudder constitute the primary control system and are required to control an aircraft safely during flight. The AP is compatible with almost any vehicle configuration (VTOLs, USVs, UGVs, etc.), including non-traditional aircraft concepts. Specific payloads/sensors can be integrated by scripting custom protocols through onboard Virtual Machines (VMs). The redundant layering provides basic functionality while ground control software is multi-platform and functions across multiple workstations in a both a wide or local area network configuration. Thanks to the AP’s distributed architecture, the system can be used in a wide variety of vehicles ranging from small quadcopter to full size converted piloted aircraft. With nearly all payloads or ready-made third-party modules, entire systems can be connected to the AP. Additionally, there are no restrictions on the number of same-type modules connected to one system, enabling multiple redundancy on all levels. This decentralized configuration helps to manage central processor loading by distributing routine management tasks across all system components. interference with the flight control system at the test site. Each component of the system has a dedicated microcontroller providing data and communication with other components within the CAN bus. stability and control derivatives were estimated for a fixed wing Unmanned Air Vehicle (UAV). All diagnostics, flight mission planning and remote control can be achieved wirelessly.Ī notable feature of the AP is its distributed architecture. Autonomous Unmanned Aerial Vehicles Control System Intellectualization. All flight systems including take-off, landing, navigation and mission execution can be instigated with a single keystroke. Navy, and Boeing, and is currently undergoing flight test at Edwards Air Force Base in California. The Automatic Control System (AP) provides the hardware and vehicle control abstraction layer for the host platform enabling fully autonomous operation. The Joint Unmanned Combat Air System (J-UCAS) X-45A is an autonomous unmanned prototype aircraft under development by DARPA, United States Air Force, U.S.
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