Navigation Strategy In-flight Retrieving and Transportation Operations for a Rotorcraft MAV

Autor: G. Flores, Juan Escareno, J. Castillo, K. Camarillo, Wafik Abassi
Přispěvatelé: Institut Polytechnique des Sciences Avancées (IPSA), Informatique, Biologie Intégrative et Systèmes Complexes (IBISC), Université d'Évry-Val-d'Essonne (UEVE), Instituto Tecnológico de Celaya, Perception and Robotics LAB, Centro de Investigaciones en Optica, Systèmes et Réseaux Intelligents (XLIM-SRI), XLIM (XLIM), Université de Limoges (UNILIM)-Centre National de la Recherche Scientifique (CNRS)-Université de Limoges (UNILIM)-Centre National de la Recherche Scientifique (CNRS), University of Barcelona, Departamento de Ingeniería Matemática [Santiago] (DIM), Universidad de Chile = University of Chile [Santiago] (UCHILE)-Centre National de la Recherche Scientifique (CNRS)
Jazyk: angličtina
Rok vydání: 2017
Předmět:
Zdroj: 4th Workshop on Research, Education and Development of Unmanned Aerial Systems (RED-UAS 2017)
4th Workshop on Research, Education and Development of Unmanned Aerial Systems (RED-UAS 2017), Oct 2017, Linköping, Sweden. (elec. proc.)
2017 Workshop on Research, Education and Development of Unmanned Aerial Systems (RED-UAS)
2017 Workshop on Research, Education and Development of Unmanned Aerial Systems (RED-UAS), Oct 2017, Linkoping, France. pp.7-12, ⟨10.1109/RED-UAS.2017.8101635⟩
HAL
DOI: 10.1109/RED-UAS.2017.8101635⟩
Popis: International audience; The paper addresses a robust navigation strategy of a rotorcraft class having a simple robotic arm to perform rapid in-flight retrieving operations in presence of wind gusts and aerodynamic effects. The target-acquiring trajectory planner is based on a cosinusoidal dynamic pattern. The mathematical model is extended to account not only the dynamics of the robotic arm but also the aerodynamics. The navigation control scheme is based on a soft integral sliding-mode control (ISC) to stabilize both inner-and outer-loop dynamics regarding the rejection of not only the dynamic couplings but also aerodynamic disturbances. Detailed simulations including realistic aerodynamic effects results show the validity of the proposed navigation strategy while tracking the object-to-retrieve trajectory.
Databáze: OpenAIRE