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Conference Program of WCICA 2012

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<strong>WCICA</strong> <strong>2012</strong><br />

Book <strong>of</strong> Abstracts: Saturday Sessions<br />

Li, Zhijun<br />

Zhai, Dihua<br />

Cao, Xiaoqing<br />

Shanghai Jiao Tong Univ.<br />

Uiversity <strong>of</strong> Sci. & Tech. <strong>of</strong> China<br />

Shanghai Jiao Tong Univ<br />

In this paper, bilateral teleoperation control is proposed for holonomic<br />

constrained robotic manipulators with stochastic time-varying delays in<br />

communication channels. A unified control model is introduced for representing<br />

well-known holonomic systems with an environmental constraint.<br />

By integrating Markov jump systems, the motion/force tracking<br />

control strategy is developed. Furthermore, a feasible solution for the<br />

derived linear matrix inequality guarantees the attenuation <strong>of</strong> unsymmetrical<br />

stochastic delay in an propobalty sense. Finally, the proposed<br />

control are validated by extensive simulation and experimental studies.<br />

◮ SaA09-2 13:50–14:10<br />

Mathematical Model Building and Optimization Control <strong>of</strong> Horizontal<br />

Continuous Heat Treatment Furnace, pp.2412–2416<br />

Hu, Lingyan<br />

Wang, Xingcheng<br />

College <strong>of</strong> Information Engineering,Dalian Univ.<br />

Dalian Maritime Unversity<br />

According to the large continuous annealing furnace widely used to produce<br />

ductile iron pipes in metallurgy area, heat transfer mathematical<br />

model was built in the paper. Based on the pipe setting temperature<br />

curve and boundary conditions, temperature distribution in the furnace<br />

is deduced by solving heat transfer differential equation. The aim is<br />

to optimize the control temperature curve. In order to make the temperature<br />

uniform in the furnace, the pulse combustion control program<br />

is developed. The actual application shows that the product quality is<br />

enhanced in a large scale with the optimization curve. The maneuverability<br />

is good. The whole system meets the process requirements<br />

perfectly. It also proves the truth and practicability <strong>of</strong> the model algorithm<br />

◮ SaA09-3 14:10–14:30<br />

Occluded Object Grasping Based on Robot Stereo Vision, pp.3698–<br />

3704<br />

Lin, Chuan<br />

Chen, Yen-Lun<br />

Hao, Weidong<br />

Wu, Xinyu<br />

Guilin Univ. <strong>of</strong> Electronic Tech.<br />

Shenzhen Inst. <strong>of</strong> Advanced Tech., Chinese Acad.<br />

<strong>of</strong> Sci.<br />

Guilin Univ. <strong>of</strong> Electronic Tech.<br />

Shenzhen Inst.s <strong>of</strong> Advacned Tech., CAS<br />

To solve the problem <strong>of</strong> occlusion for robot grasping, a novel method is<br />

proposed, by which the robot can grasp an occluded target object accurately.<br />

In this paper, the principles <strong>of</strong> binocular vision, camera calibration,<br />

stereo rectification and stereo matching are described. By utilizing<br />

the stereo-vision algorithm, robots can obtain the three-dimensional information<br />

<strong>of</strong> objects. For accurate grasping, the depth information <strong>of</strong><br />

the object is optimized, where the principles <strong>of</strong> connected consistency<br />

and threshold setting have been applied in the depth image. The ORB<br />

algorithm is applied to find the occlusion dynamically. The approach for<br />

grasping the occluded object is proved to be effective by experiments.<br />

◮ SaA09-4 14:30–14:50<br />

Intelligent Switching Control for Cement Raw Meal Calcination Process,<br />

pp.280–285<br />

Qiao, Jinghui<br />

Chai, Tian-you<br />

Northeastern Univ.<br />

Northeastern Univ.<br />

In raw meal calcination process, since boundary conditions <strong>of</strong> raw meal<br />

change frequently, the decomposition rate <strong>of</strong> raw meal (RMDR) cannot<br />

guarantee the desirable ranges. Therefore, C5 feeding tube was<br />

blocked and the load <strong>of</strong> rotary kiln will increase. To solve above problem,<br />

an intelligent switching control method is proposed to control the<br />

calciner temperature into their setpoints. This method for raw meal calcination<br />

process consists <strong>of</strong> four modules, namely a easy calcination<br />

controller, a difficult calcination controller, a abnormal condition controller,<br />

and a switching mechanism. The proposed approach can select<br />

right controller according to the change <strong>of</strong> the working conditions and<br />

has been successfully applied to the raw meal calcination process <strong>of</strong><br />

Jiuganghongda Cement Plant in China and its efficiency has been validated<br />

by the practical application results.<br />

◮ SaA09-5 14:50–15:10<br />

Design <strong>of</strong> Entry Trajectory Tracking Law for a Hypersonic Vehicle via<br />

Inversion Control, pp.1092–1097<br />

Pu, Zhiqiang<br />

Tan, Xiangmin<br />

Fan, Guoliang<br />

Yi, Jian-qiang<br />

Inst. <strong>of</strong> Automation, Chinese Acad. <strong>of</strong> Sci.<br />

Inst. <strong>of</strong> Automation, Chinese Acad. <strong>of</strong> Sci.<br />

Inst. <strong>of</strong> Automation, Chinese Acad. <strong>of</strong> Sci.<br />

Inst. <strong>of</strong> automation, chinese Acad. <strong>of</strong> Sci.<br />

A nominal altitude-velocity longitudinal entry trajectory is planned and<br />

tracked for a Generic Hypersonic Vehicle (GHV) in this paper. The entry<br />

corridor is presented which is defined by the dynamic pressure, normal<br />

acceleration, heating constraints, and the so-called Quasi-Equilibrium<br />

Glide Condition (QEGC). The flyability <strong>of</strong> the vehicle along the nominal<br />

trajectory is carefully analyzed for further validation <strong>of</strong> the selected<br />

nominal trajectory. The control scheme mainly consists <strong>of</strong> two loops: a<br />

guidance loop and a posture loop, <strong>of</strong> which the latter is separated into<br />

the slow and fast loops with the time-scale separation theory. Inversion<br />

control is employed in these three loops, and an integration feedback<br />

approach is especially added into the inversion controller to eliminate<br />

the tracking error. Simulations demonstrate that the nominal trajectory<br />

is designed appropriately and tracked well.<br />

◮ SaA09-6 15:10–15:30<br />

Finite-Horizon Neural Optimal Tracking Control for a Class <strong>of</strong> Nonlinear<br />

Systems with Unknown Dynamics, pp.138–143<br />

Wang, Ding<br />

Liu, Derong<br />

Li, Hongliang<br />

Inst. <strong>of</strong> Automation, Chinese Acad. <strong>of</strong> Sci.<br />

CASIA<br />

chinese Acad. <strong>of</strong> Sci.<br />

A neural-network-based finite-horizon optimal tracking control scheme<br />

for a class <strong>of</strong> unknown nonlinear discrete-time systems is proposed.<br />

First, the tracking control problem is converted into designing a regulator<br />

for the tracking error dynamics under the framework <strong>of</strong> finite-horizon<br />

optimal control theory. Then, with convergence analysis in terms <strong>of</strong> cost<br />

function and control law, the iterative adaptive dynamic programming<br />

algorithm is introduced to obtain the finite horizon optimal controller to<br />

make the cost function close to its optimal value within an ”-error bound.<br />

Furthermore, in order to implement the algorithm via dual heuristic dynamic<br />

programming technique, three neural networks are employed to<br />

approximate the error dynamics, the cost function, and the control law,<br />

respectively. In addition, a numerical example is given to demonstrate<br />

the validity <strong>of</strong> the present approach.<br />

SaA10 13:30–15:30 Room 311B<br />

Invited Session: Guidance and Control <strong>of</strong> Flight Vehicles: Theory and<br />

Application<br />

Chair: He, Fenghua<br />

Co-Chair: Liu, Fuchun<br />

Harbin Inst. <strong>of</strong> Tech.<br />

South China Univ. <strong>of</strong> Tech.<br />

◮ SaA10-1 13:30–13:50<br />

Square Division Method for Attitude Dynamic Analysis <strong>of</strong> Modular S-<br />

pace Station, pp.1350–1355<br />

Guo, Jian<br />

Guo, Yang<br />

Zhang, Peng<br />

Yao, Yu<br />

Zhao, Hui<br />

Yang, Baoqing<br />

Harbin Inst. <strong>of</strong> Tech.<br />

Harbin Inst. <strong>of</strong> Tech.<br />

Harbin Inst. <strong>of</strong> Tech.<br />

Harbin Inst. <strong>of</strong> Tech.<br />

Harbin Inst. <strong>of</strong> Tech.<br />

Harbin Inst. <strong>of</strong> Tech.<br />

This paper presents a numerical method to calculate the aerodynamic<br />

force and torque for the complex spacecraft considering components<br />

blocking. The Square Division Method (SDM) is applied to<br />

analyze and therefore evaluate the space station’s structure. The<br />

efficiency and accuracy <strong>of</strong> the SDM are investigated in the simulation<br />

section primarily. Then major structures <strong>of</strong> the space station are<br />

analyzed and evaluated by testing their performance in the Local-<br />

Horizontal-Local-Vertical (LVLH), Inertial-Oriented-Attitude (IOA) and<br />

Torque-Equilibrium-Attitude (TEA) modes. The long-term momentum<br />

accumulation is chosen as the criterion to evaluate appropriate flight<br />

modes for each structure. Based on the simulation results, appropriate<br />

operation modes are decided for each structure.<br />

155

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