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Secure Command and Control Link with Interference Mitigation ( PDF) Purpose: The Control Non-Payload Communication ( CNPC) flight demonstration will prove the feasibility of using a small radio in a small Unmanned Aircraft Systems ( sUAS) airframe that allows flexible employment of sUAS, and answers the following question: Can a radio developed based on the RTCA Minimum Operational and Performance Standards ( MOPS) be practical to use for all sUAS? Purpose: The certification test case will validate small Unmanned Aircraft Systems ( sUAS) industry standards and support standards development and certification strategies for sUAS, necessary for their safe integration in the National Airspace System ( NAS).Ĭontrol Non-Payload Communication Testing for Unmanned Aircraft Systems ( PDF)
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How can the design of a UAS minimize potential damage during a ground collision?.What is the severity of a UAS collision with person or property on the ground?.What are the severity criteria for Unmanned Aircraft System ( UAS) collisions, such as weight, kinetic energy, etc.?.Purpose: The Unmanned Aircraft System ( UAS) Ground Collision Severity Evaluation study will provide data to help inform: Unmanned Aircraft Systems Ground Collision Severity Evaluation ( PDF) One-page status reports on research conducted or being conducted regarding the safe integration of unmanned aircraft systems ( UAS) into the National Airspace System ( NAS). Recreational Flyers & Modeler Community-Based Organizations.Critical Infrastructure & Public Venues.Certificated Remote Pilots including Commercial Operators.Legislation & Policies, Regulations & Guidance.
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Data & Research Subnav: Data & Research 1.Airport Safety Information Video Series.Passenger Facility Charge (PFC) Program.Airport Coronavirus Response Grant Program.General Aviation & Recreational Aircraft.Vintage & Experimental Aircraft Program.Aviation Safety Draft Documents Open for Comment.Furthermore, this paper may also focuses on the review research involved with the design modification and the generated flow phenomena of Micro air vehicle MAV. This report provides an overview on the state of unmanned air vehicle and introduces the techniques of Active Flow Control ACF that could be potentially used for control of UAV. The investigation and research in this field is rapidly rising and there are many concepts currently being considered around the world. Improved aerodynamic performance of these air vehicles can lead to fast take off and slower landing speeds that can be related to reduce noise and crash survivability issues. A good example is the Coandă MAV which uses the Active flow control-Coandă Effect. This has led to the development of novel platforms that move away from traditional aircraft design in order to make them more capable. In order to carry out a task, these air vehicles have to face many different challenges, due to the MAVs small size, flight regime, and modes of operation. Sophisticated unmanned air vehicles for general applications have been developed rapidly across many different industries and interested researchers. These air vehicles have the potential to revolutionize our sensing and information gathering capabilities, in homeland security and environmental areas. Coandă effect can be found in virtually all aerodynamic applications, and has drawn renewed interest for various applications, among others for generating lift and maneuvering impulses to be applied for unmanned air vehicles (UAV) and micro air vehicles (MAV).