The Experts below are selected from a list of 2865 Experts worldwide ranked by ideXlab platform
Nikolajs Glīzde - One of the best experts on this subject based on the ideXlab platform.
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Plotting the Flight Envelope of an Unmanned Aircraft System Air Vehicle
Transport and Aerospace Engineering, 2017Co-Authors: Nikolajs GlīzdeAbstract:Abstract The research is focused on the development of an Unmanned Aircraft System. One of the design process steps in the preliminary design phase is the calculation of the flight envelope for the Unmanned Aircraft System air vehicle. The results obtained will be used in the further design process. A flight envelope determines the minimum requirements for the object in Certification Specifications. The present situation does not impose any Certification Specification requirements for the class of the Unmanned Aircraft System under the development of the general European Union trend defined in the road map for the implementation of the Unmanned Aircraft System. However, operation in common European Aerospace imposes the necessity for regulations for micro class systems as well.
H Fluhr - One of the best experts on this subject based on the ideXlab platform.
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proposal of a Certification Specification for a light unmanned aerial system cs luas
2013Co-Authors: F Glatzl, G Lippitsch, H FluhrAbstract:Unmanned Aerial Systems (UAS) are a rising field of interest in aviation. Besides military applications where UAS have been operated for years in 4D (Dull, Dangerous, Dirty and Deep) missions, civil applications are stagnating. The development of civil Light Unmanned Aerial Systems and their integration into civil aerospace is presently a topic of interest for National Aviation Agencies and International Aviation Organizations. While large UASs will be covered by an EASA-building code, the design approval of light drones (Class I and Class II) will remain in the jurisdiction of National Aviation Authorities. To insure a homogeneous procedural method, the Joint Aviation Authorities (JAR) founded the task group Joint Authorities for Rulemaking on Unmanned Systems (JARUS) with the aim to acquire and to agree on a basic prescription. In a preliminary investigation, a Certification Specification for Light Unmanned Aerial Systems (CS-LUAS) was developed in order to ensure a common and easy Certification process for Unmanned Aerial Vehicles with a maximum takeoff weight of 150kg, the ground control unit and the command and control datalink. The tailoring principle was applied in order to obtain the building code. The Certification Specification for Very Light Aeroplanes (CS-VLA) was chosen as a baseline and every paragraph was reviewed and evaluated concerning its applicability for UASs. Besides the mentioned Certification Specification, the NATO Standardization Agreement STANAG 4671 was incorporated to cover aspects like the departure, landing and equipment that is necessary for a safe operation of the unmanned system. The proposed draft of a Certification Specification for Light Unmanned Systems will be reviewed in the JARUS task group and will contribute to the development of a pan-European building code for light UAS.
Don Harris - One of the best experts on this subject based on the ideXlab platform.
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Human factors for flight deck Certification: Issues in compliance with the new European aviation safety agency Certification Specification 25.1302
Journal of aeronautics astronautics and aviation Series A, 2010Co-Authors: Don HarrisAbstract:In September 2007 EASA (European Aviation Safety Agency) implemented a new airworthiness rule (CS 25.1302) that mandates for the error tolerant design of flight deck equipment on all new large commercial aircraft. The stimulus for the rule was the 1996 FAA Human Factors Team Report on the Interfaces between Flightcrews and Modern Flight Deck Systems, which was commissioned as a result of several accidents occurring to new (at the time) technology airliners. This report made many criticisms of the flight deck interfaces and design processes, including a lack of human factors expertise on design teams and too much emphasis being placed on the physical ergonomics of the pilot’s workplace and not on the cognitive ergonomics. This paper provides a very brief overview of the concept of design-induced error and the background to the rule, before providing a brief summary of the acceptable means of compliance with the regulation and providing a brief critique of the criteria of the related measurement instruments and methods available.
F Glatzl - One of the best experts on this subject based on the ideXlab platform.
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proposal of a Certification Specification for a light unmanned aerial system cs luas
2013Co-Authors: F Glatzl, G Lippitsch, H FluhrAbstract:Unmanned Aerial Systems (UAS) are a rising field of interest in aviation. Besides military applications where UAS have been operated for years in 4D (Dull, Dangerous, Dirty and Deep) missions, civil applications are stagnating. The development of civil Light Unmanned Aerial Systems and their integration into civil aerospace is presently a topic of interest for National Aviation Agencies and International Aviation Organizations. While large UASs will be covered by an EASA-building code, the design approval of light drones (Class I and Class II) will remain in the jurisdiction of National Aviation Authorities. To insure a homogeneous procedural method, the Joint Aviation Authorities (JAR) founded the task group Joint Authorities for Rulemaking on Unmanned Systems (JARUS) with the aim to acquire and to agree on a basic prescription. In a preliminary investigation, a Certification Specification for Light Unmanned Aerial Systems (CS-LUAS) was developed in order to ensure a common and easy Certification process for Unmanned Aerial Vehicles with a maximum takeoff weight of 150kg, the ground control unit and the command and control datalink. The tailoring principle was applied in order to obtain the building code. The Certification Specification for Very Light Aeroplanes (CS-VLA) was chosen as a baseline and every paragraph was reviewed and evaluated concerning its applicability for UASs. Besides the mentioned Certification Specification, the NATO Standardization Agreement STANAG 4671 was incorporated to cover aspects like the departure, landing and equipment that is necessary for a safe operation of the unmanned system. The proposed draft of a Certification Specification for Light Unmanned Systems will be reviewed in the JARUS task group and will contribute to the development of a pan-European building code for light UAS.
G Lippitsch - One of the best experts on this subject based on the ideXlab platform.
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proposal of a Certification Specification for a light unmanned aerial system cs luas
2013Co-Authors: F Glatzl, G Lippitsch, H FluhrAbstract:Unmanned Aerial Systems (UAS) are a rising field of interest in aviation. Besides military applications where UAS have been operated for years in 4D (Dull, Dangerous, Dirty and Deep) missions, civil applications are stagnating. The development of civil Light Unmanned Aerial Systems and their integration into civil aerospace is presently a topic of interest for National Aviation Agencies and International Aviation Organizations. While large UASs will be covered by an EASA-building code, the design approval of light drones (Class I and Class II) will remain in the jurisdiction of National Aviation Authorities. To insure a homogeneous procedural method, the Joint Aviation Authorities (JAR) founded the task group Joint Authorities for Rulemaking on Unmanned Systems (JARUS) with the aim to acquire and to agree on a basic prescription. In a preliminary investigation, a Certification Specification for Light Unmanned Aerial Systems (CS-LUAS) was developed in order to ensure a common and easy Certification process for Unmanned Aerial Vehicles with a maximum takeoff weight of 150kg, the ground control unit and the command and control datalink. The tailoring principle was applied in order to obtain the building code. The Certification Specification for Very Light Aeroplanes (CS-VLA) was chosen as a baseline and every paragraph was reviewed and evaluated concerning its applicability for UASs. Besides the mentioned Certification Specification, the NATO Standardization Agreement STANAG 4671 was incorporated to cover aspects like the departure, landing and equipment that is necessary for a safe operation of the unmanned system. The proposed draft of a Certification Specification for Light Unmanned Systems will be reviewed in the JARUS task group and will contribute to the development of a pan-European building code for light UAS.