2,399 research outputs found
Modeling, Stability Analysis, and Testing of a Hybrid Docking Simulator
A hybrid docking simulator is a hardware-in-the-loop (HIL) simulator that
includes a hardware element within a numerical simulation loop. One of the
goals of performing a HIL simulation at the European Proximity Operation
Simulator (EPOS) is the verification and validation of the docking phase in an
on-orbit servicing mission.....Comment: 30 papge
Energy-based Modeling and Control of Interactive Aerial Robots:A Geometric Port-Hamiltonian Approach
A review of aerial manipulation of small-scale rotorcraft unmanned robotic systems
Small-scale rotorcraft unmanned robotic systems (SRURSs) are a kind of unmanned rotorcraft with manipulating devices. This review aims to provide an overview on aerial manipulation of SRURSs nowadays and promote relative research in the future. In the past decade, aerial manipulation of SRURSs has attracted the interest of researchers globally. This paper provides a literature review of the last 10 years (2008–2017) on SRURSs, and details achievements and challenges. Firstly, the definition, current state, development, classification, and challenges of SRURSs are introduced. Then, related papers are organized into two topical categories: mechanical structure design, and modeling and control. Following this, research groups involved in SRURS research and their major achievements are summarized and classified in the form of tables. The research groups are introduced in detail from seven parts. Finally, trends and challenges are compiled and presented to serve as a resource for researchers interested in aerial manipulation of SRURSs. The problem, trends, and challenges are described from three aspects. Conclusions of the paper are presented, and the future of SRURSs is discussed to enable further research interests
Design and control of next-generation uavs for effectively interacting with environments
In this dissertation, the design and control of a novel multirotor for aerial manipulation is studied, with the aim of endowing the aerial vehicle with more degrees of freedom of motion and stability when interacting with the environments. Firstly, it presents an energy-efficient adaptive robust tracking control method for a class of fully actuated, thrust vectoring unmanned aerial vehicles (UAVs) with parametric uncertainties including unknown moment of inertia, mass and center of mass, which would occur in aerial maneuvering and manipulation. The effectiveness of this method is demonstrated through simulation. Secondly, a humanoid robot arm is adopted to serve as a 6-degree-of-freedom (DOF) automated flight testing platform for emulating the free flight environment of UAVs while ensuring safety. Another novel multirotor in a tilt-rotor architecture is studied and tested for coping with parametric uncertainties in aerial maneuvering and manipulation. Two pairs of rotors are mounted on two independently-controlled tilting arms placed at two sides of the vehicle in a H configuration to enhance its maneuverability and stability through an adaptive robust control method. In addition, an impedance control algorithm is deployed in the out loop that modifies the trajectory to achieve a compliant behavior in the end-effector space for aerial drilling and screwing tasks
Six-DOF Spacecraft Dynamics Simulator For Testing Translation and Attitude Control
This paper presents a method to control a manipulator system grasping a
rigid-body payload so that the motion of the combined system in consequence of
externally applied forces to be the same as another free-floating rigid-body
(with different inertial properties). This allows zero-g emulation of a scaled
spacecraft prototype under the test in a 1-g laboratory environment. The
controller consisting of motion feedback and force/moment feedback adjusts the
motion of the test spacecraft so as to match that of the flight spacecraft,
even if the latter has flexible appendages (such as solar panels) and the
former is rigid. The stability of the overall system is analytically
investigated, and the results show that the system remains stable provided that
the inertial properties of two spacecraft are different and that an upperbound
on the norm of the inertia ratio of the payload to manipulator is respected.
Important practical issues such as calibration and sensitivity analysis to
sensor noise and quantization are also presented
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