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Design and realization of hybrid ACO-based PID and LuGre friction compensation controller for three degree-of-freedom high precision flight simulator
Authors:Haibin Duan  Senqi Liu  Daobo Wang  Xiufen Yu
Affiliation:1. School of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, PR China;2. College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, PR China;3. Center for Space Science and Applied Research, Chinese Academy of Sciences, Beijing 100190, PR China;1. DOE National Energy Technology Laboratory, 1450 Queen Ave., SW, Albany, OR 97321, USA;2. URS Corp., P.O. Box 1959, Albany, OR 97321, USA;3. DOE National Energy Technology Laboratory, Cochrans Mill Rd., P.O. Box 10940, Pittsburgh, PA 15236, USA;1. Department of Cardiovascular Surgery, University of Tsukuba, Ibaraki, Japan;2. Department of Pediatric Cardiology, University of Tsukuba, Ibaraki, Japan;1. School of Electro-Mechanical Engineering, Xidian University, Xi''an 710071, China;2. School of Electronic Engineering, Xidian University, Xi''an 710071, China;1. Istituto Italiano di Tecnologia, Robotics, Brain and Cognitive Sciences Department, Via Morego 30, Genova 16163, Italy;2. Istituto Italiano di Tecnologia, Graphene Labs, Via Morego 30, Genova 16163, Italy;3. Istituto Italiano di Tecnologia, Smart Materials, Via Morego 30, Genova 16163, Italy
Abstract:Three degree-of-freedom (3-DOF) high precision flight simulator is a type of key hardware-in-loop equipment in the fields of aeronautics and astronautics. The conventional Proportional–Integral–Derivative (PID) is a widely used industrial controller that uses a combination of proportional, integral and derivative action on the control error to form the output of the controller. It is well known that the undesired phenomena caused by friction can lead to overall flight simulator performance degradation or instability. This paper presents a novel kind of hybrid Ant Colony Optimization (ACO)-based PID and LuGre friction compensation controller for 3-DOF high precision flight simulator. On the basis of introduction of the basic principles of ACO, the controlling scheme design for the 3-DOF high precision flight simulator is presented. Based on the popular LuGre friction model, a novel nonlinear friction compensation controller for 3-DOF high precision flight simulator is also developed. The proposed Lyapunov function proves the robust global convergence of the tracking error. The parameters tuning of PID can be summed up as the typical continual spatial optimization problem, grid-based searching strategy is adopted in the improved ACO algorithm, and self-adaptive control strategy for the pheromone decay parameter is also adopted. Modularization design is adopted in the 3-DOF high precision flight simulator. This software can process the position and status signals, and display them on the friendly interface. Double buffer mechanism is adopted in the communication protocol between lower Industrial Personal Computer (IPC) and upper IPC. The series experimental results have verified the feasibility and effectiveness of the proposed hybrid ACO-based PID and LuGre friction compensation controller.
Keywords:
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