Results 11 to 20 of about 3,306,168 (280)
Wake Vortex Modelling and Simulation for Air Vehicles in Close Formation Flight [PDF]
, 2010 The aim of this research is to develop realistic models of aerodynamic cross-coupling e ects that can be incorporated in real-time or near real-time simulations of Unmanned Aerial Vehicles (UAVs) in close formation flight.
Saban, Deborah
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Advances in understanding autogyro flight dynamics [PDF]
, 2008 A comprehensive flight dynamics study of the autogyro is presented in this paper. A state of the art generic simulation of the vehicle type was developed and validated against flight data.
Thomson, D.G., Houston, S.
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Design and Integration of a Tilt-Rotor Flight Simulation Platform [PDF]
, 2022 This paper introduces a tilt-rotor flight simulation platform for research and teaching purposes implementing a real-time simulation of the Bell XV-15 aircraft. The mathematical model of the XV-15 aircraft has been implemented including simplified models
Guglieri, Giorgio +7 more
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Development of ground station display and flight management system for low-cost vehicle [PDF]
, 2011 Nowadays, with the development of electronic and communication technologies, more and more low-cost vehicles such as small, light-weight aircraft are widely applied in all kinds of fields.
Pan, Jing
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Simulation of wake vortex effects for UAVs in close formation flight [PDF]
, 2009 This paper addresses the development of multiple UAV deployment simulation models that include representative aerodynamic cross-coupling effects. Applications may include simulations of autonomous aerial refuelling and formation flying scenarios.
Whidborne, James F. +2 more
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Development of real-time flight control system for low-cost vehicle [PDF]
, 2011 In recent years, more and more light aircraft enter our daily life, from Agricultural applications, emergency rescue, flight experiment and training to Barriers to entry, light aircraft always have their own advantages. Thus, they have become more and
Du, Yongliang
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Научный вестник МГТУ ГА, 2023 Due to a steady extension of the flight envelope of modern agile combat aircraft, with the growing requirements for state tests, it is increasingly necessary to study the entire flight envelope and specifically, to determine the main performance data of ...
K. A. Zhuravsky, P. S. Kostin
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Development of Aerodynamic and Propulsion Models Using the Iterative Equation Error Method
Aerospace, 2023 For developing high-fidelity flight simulations, an accurate and complete representation of the aerodynamic characteristics of the aircraft is necessary.
Murat Millidere +3 more
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Aerospace, 2020 Collisions between birds and aircraft pose a severe threat to aviation and avian safety. To understand and prevent these bird strikes, knowledge about the factors leading to these bird strikes is vital.
Isabel C. Metz +4 more
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Evaluation method of privacy protection effect based on multi-layer fuzzy comprehensive evaluation
网络与信息安全学报, 2020 Aiming at the problem that the evaluation of the privacy protection effect from a single data level cannot describe the overall privacy protection effect of the network environment, with the help of the fuzzy comprehensive evaluation method, the privacy
YU Yihan, FU Yu, WU Xiaoping
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