Rotorcraft with a 3DOF Rigid Manipulator: Quaternion-based Modeling and Real-time Control Tolerant to Multi-body Couplings

被引:9
作者
Alvarez-Munoz, J. [1 ]
Marchand, N. [2 ]
Guerrero-Castellanos, J. F. [3 ]
Tellez-Guzman, J. J. [2 ]
Escareno, J. [4 ]
Rakotondrabe, M. [5 ]
机构
[1] Polytech Inst Adv Sci, FR-94200 Paris, France
[2] Univ Grenoble Alpes, GIPSA Lab, FR-38000 Grenoble, France
[3] Autonomous Univ Puebla BUAP, Fac Elect, MX-72570 Puebla, Mexico
[4] Univ Limoges ENSIL ENSCI, XLIM Lab, UMR CNRS 7252, Parc Ester Technopole,16 Rue Atlantis, F-87068 Limoges, France
[5] FEMTO ST Inst, UMR CNRS UFC ENSMM UTBM, Automat Control & Micromechatron Dept, Fr Besancon, France
关键词
Observer-based control; quaternion and Newton-Euler modeling; bounded-input control; aerial manipulator; disturbance rejection;
D O I
10.1007/s11633-018-1145-8
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper proposes a simple solution for the stabilization of a mini-quadcopter carrying a 3DoF (degrees of freedom) manipulator robot in order to enhance its achievable workspace and application profile. Since the motion of the arm induces torques which degrade the stability of the system, in the present work, we consider the stabilization of both subsystems: the quadcopter and the robotic arm. The mathematical model of the system is based on quaternions. Likewise, an attitude control law consisting of a bounded quaternion-based feedback stabilizes the quadcopter to a desired attitude while the arm is evolving. The next stage is the translational dynamics which is simplified for control (nonlinear) design purposes. The aforementioned controllers are based on saturation functions whose stability is explicitly proved in the Lyapunov sense. Finally, experimental results and a statistical study validate the proposed control strategy.
引用
收藏
页码:547 / 558
页数:12
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