This study describes the application of the task priority null-space behavioural technique to the coordinated controlof a team of flying vehicles with hovering capabilities, such as helicopters or quadrotors, in the presence of obstacles andno-fly zones. Once a flight mission is assigned to the team in terms of a target region to reach, each flying vehicle is required toaccomplish four tasks with assigned priorities. Formation flight and collisions avoidance with other vehicles and unknown ormoving obstacles tasks are formulated via analytical expressions as required by the classical null-space behavioural approach.Move to target and a priori known obstacle avoidance behaviours are obtained by solving a partial differential equationproblem within the flight domain. The effectiveness of the proposed technique is discussed with regards to two-dimensionaland three-dimensional numerical examples.

Task priority approach to the coordinated control of a team of flying vehicles in the presence of obstacles / Mattei, M; Scordamaglia, Valerio. - In: IET CONTROL THEORY & APPLICATIONS. - ISSN 1751-8644. - 6:13(2012), pp. 2103-2110. [10.1049/iet-cta.2010.0742]

Task priority approach to the coordinated control of a team of flying vehicles in the presence of obstacles

SCORDAMAGLIA, Valerio
2012-01-01

Abstract

This study describes the application of the task priority null-space behavioural technique to the coordinated controlof a team of flying vehicles with hovering capabilities, such as helicopters or quadrotors, in the presence of obstacles andno-fly zones. Once a flight mission is assigned to the team in terms of a target region to reach, each flying vehicle is required toaccomplish four tasks with assigned priorities. Formation flight and collisions avoidance with other vehicles and unknown ormoving obstacles tasks are formulated via analytical expressions as required by the classical null-space behavioural approach.Move to target and a priori known obstacle avoidance behaviours are obtained by solving a partial differential equationproblem within the flight domain. The effectiveness of the proposed technique is discussed with regards to two-dimensionaland three-dimensional numerical examples.
2012
aircraft control, partial differential equations, collision avoidance
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/20.500.12318/8169
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