Robust Guidance Strategy for Target Circulation by Controlled UAV

A controlled fixed-wing unmanned aerial vehicle is modeled as a simplified low-dimensional nonlinear dynamical system with additive disturbances. The guidance strategy presented, considering simultaneously inputs and states constraints, is shown to be robust to additive perturbations representing no...

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Bibliographic Details

Published in:	IEEE transactions on aerospace and electronic systems Vol. 54; no. 3; pp. 1415 - 1431
Main Authors:	Gomes Olavo, Jose Lucas, Thums, Goncalo Daniel, Jesus, Tales Argolo, Cunha de Araujo Pimenta, Luciano, Borges Torres, Leonardo Antonio, Martinez Palhares, Reinaldo
Format:	Journal Article
Language:	English
Published:	IEEE 01-06-2018
Subjects:	Aerodynamics Aircraft Artificial vector field Atmospheric modeling fixed-wing unmanned aerial vehicle (UAV) inputs and states constraints Mathematical model robust guidance Robustness target circulation Uncertainty Vehicle dynamics
Online Access:	Get full text
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