Optimal 3D trajectory generation in delivering missions under urban constraints for a flying robot
Interest in applying flying robots especially quadcopters for civil applications, in particular for delivering purposes, has dramatically grown in the recent years. In fact, since quadcopters are capable of vertical takeoff and landing, they can be widely employed for nearly any aerial task where a...
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Veröffentlicht in: | Intelligent service robotics 2017-07, Vol.10 (3), p.241-256 |
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description | Interest in applying flying robots especially quadcopters for civil applications, in particular for delivering purposes, has dramatically grown in the recent years. In fact, since quadcopters are capable of vertical takeoff and landing, they can be widely employed for nearly any aerial task where a human presence is hazardous or response time is critical. In this regard, quadcopters come to be very beneficial in delivering packages; accordingly, generating an optimal flight trajectory plays a preponderant role for meeting this vision. This paper is concerned with generation of a time-optimal 3D path for a quadcopter under municipal restrictions in delivering tasks. To this end, the flying robot’s dynamics is first modeled through Newton–Euler method. Subsequently, the problem is formulated as a time-optimal control problem such that the urban constraints, which are safe-margins of high-rise buildings located throughout the course, are first modeled and then imposed to the trajectory optimization problem as inequality constraints. After discretizing the trajectory by means of Hermit–Simpson method, the optimal control problem is transformed into a nonlinear programming problem and finally is solved by the direct collocation technique. Extensive simulations demonstrate the efficacy of the proposed method and correspondingly verify the effectiveness of the suggested method in generation of optimum 3D routes while all constraints and mission requirements are satisfied. |
doi_str_mv | 10.1007/s11370-017-0225-x |
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Subsequently, the problem is formulated as a time-optimal control problem such that the urban constraints, which are safe-margins of high-rise buildings located throughout the course, are first modeled and then imposed to the trajectory optimization problem as inequality constraints. After discretizing the trajectory by means of Hermit–Simpson method, the optimal control problem is transformed into a nonlinear programming problem and finally is solved by the direct collocation technique. 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A. Amiri</creatorcontrib><title>Optimal 3D trajectory generation in delivering missions under urban constraints for a flying robot</title><title>Intelligent service robotics</title><addtitle>Intel Serv Robotics</addtitle><description>Interest in applying flying robots especially quadcopters for civil applications, in particular for delivering purposes, has dramatically grown in the recent years. In fact, since quadcopters are capable of vertical takeoff and landing, they can be widely employed for nearly any aerial task where a human presence is hazardous or response time is critical. In this regard, quadcopters come to be very beneficial in delivering packages; accordingly, generating an optimal flight trajectory plays a preponderant role for meeting this vision. This paper is concerned with generation of a time-optimal 3D path for a quadcopter under municipal restrictions in delivering tasks. To this end, the flying robot’s dynamics is first modeled through Newton–Euler method. Subsequently, the problem is formulated as a time-optimal control problem such that the urban constraints, which are safe-margins of high-rise buildings located throughout the course, are first modeled and then imposed to the trajectory optimization problem as inequality constraints. After discretizing the trajectory by means of Hermit–Simpson method, the optimal control problem is transformed into a nonlinear programming problem and finally is solved by the direct collocation technique. 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Amiri</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c316t-f599b5c26132a93c18017941104c26d6f01c5996a3e4316736c499ce888062ee3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2017</creationdate><topic>Artificial Intelligence</topic><topic>Control</topic><topic>Control algorithms</topic><topic>Controllers</topic><topic>Dynamical Systems</topic><topic>Engineering</topic><topic>Equilibrium</topic><topic>Flight</topic><topic>Helicopters</topic><topic>High rise buildings</topic><topic>Mechatronics</topic><topic>Nonlinear programming</topic><topic>Optimization techniques</topic><topic>Ordinary differential equations</topic><topic>Original Research Paper</topic><topic>Planning</topic><topic>Robotics</topic><topic>Robotics and Automation</topic><topic>Robots</topic><topic>Space missions</topic><topic>Teams</topic><topic>Time optimal control</topic><topic>Trajectory optimization</topic><topic>Unmanned aerial vehicles</topic><topic>User Interfaces and Human Computer Interaction</topic><topic>Vehicles</topic><topic>Vertical takeoff</topic><topic>Vibration</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Lavaei, Abolfazl</creatorcontrib><creatorcontrib>Atashgah, M. 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In this regard, quadcopters come to be very beneficial in delivering packages; accordingly, generating an optimal flight trajectory plays a preponderant role for meeting this vision. This paper is concerned with generation of a time-optimal 3D path for a quadcopter under municipal restrictions in delivering tasks. To this end, the flying robot’s dynamics is first modeled through Newton–Euler method. Subsequently, the problem is formulated as a time-optimal control problem such that the urban constraints, which are safe-margins of high-rise buildings located throughout the course, are first modeled and then imposed to the trajectory optimization problem as inequality constraints. After discretizing the trajectory by means of Hermit–Simpson method, the optimal control problem is transformed into a nonlinear programming problem and finally is solved by the direct collocation technique. Extensive simulations demonstrate the efficacy of the proposed method and correspondingly verify the effectiveness of the suggested method in generation of optimum 3D routes while all constraints and mission requirements are satisfied.</abstract><cop>Berlin/Heidelberg</cop><pub>Springer Berlin Heidelberg</pub><doi>10.1007/s11370-017-0225-x</doi><tpages>16</tpages></addata></record> |
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subjects | Artificial Intelligence Control Control algorithms Controllers Dynamical Systems Engineering Equilibrium Flight Helicopters High rise buildings Mechatronics Nonlinear programming Optimization techniques Ordinary differential equations Original Research Paper Planning Robotics Robotics and Automation Robots Space missions Teams Time optimal control Trajectory optimization Unmanned aerial vehicles User Interfaces and Human Computer Interaction Vehicles Vertical takeoff Vibration |
title | Optimal 3D trajectory generation in delivering missions under urban constraints for a flying robot |
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