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result(s) for
"Sadraey, Mohammad H"
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Aircraft design : a systems engineering approach
\"Presenting in one volume the methodologies behind aircraft design, this book uses a systems engineering approach to cover the components and the issues affected by design procedures. The basic topics that are essential to the process, such as aerodynamics and controls, are covered first of all. The author then explains the design process in a holistic manner to emphasize the integration of individual components into the overall design. Throughout the book, the various design options are considered and weighed against each other, to give readers a practical understanding of the process overall\"-- Provided by publisher.
Optimal control and line-of-sight guidance formation flight
2013
Purpose - The purpose of this paper is to design an integrated guidance and control design for a formation flight of four unmanned aerial vehicles to follow a moving ground target.Design methodology approach - The guidance law is based on the line-of-sight. The control is optimal. The guidance law is integrated with the optimal control law and is applied to a linear dynamic model.Findings - The theoretical results are supported by the numerical simulations that illustrate a coordinated encirclement of a ground maneuvering target.Research limitations implications - A linear dynamic UAV model and a liner engine model were employed.Practical implications - This is expected to provide efficient coordination technique required in many civilian circular formation UAV applications; also the technique can be used to provide a safe environment required for the civil applications.Social implications - The research will facilitate the deployment of autonomous unmanned aircraft systems in various civilian applications such as border monitoring.Originality value - The research addresses the challenges of coordination of multiple unmanned aerial vehicles in a circular formation using an integrated optimal control technique with line-of-sight guidance.
Journal Article
Aircraft performance : an engineering approach
\"Flight is the process in which a vehicle moves through the air without any direct mechanical support from the ground. In Physics, science of the action of forces on material bodies is referred to as Mechanics. The science of \"Mechanics\" is basically divided into two branches: 1. Dynamics, and 2. Statics. Branch of mechanics that deals with the motion of objects in relation to force, mass, momentum, and energy is referred to as Dynamics. The topic of flight mechanics (or Flight Dynamics) is to study the motion of flying objects (e.g., aircraft, missile) through air\"-- Provided by publisher.