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Titlebook: System Simulation and Scientific Computing; International Confer Tianyuan Xiao,Lin Zhang,Shiwei Ma Conference proceedings 2012 Springer-Ver

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Trajectory Tracking Controller of Small-Scale Helicopter Based on Backstepping the translational dynamics and the rotational dynamics through solving an equation when the desired yaw angle is predefined. Simulation results show that the performance of the proposed controller is acceptable.
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Fuzzy Sliding Mode Variable Structure Controller for Hypersonic Cruise Vehiclee variable structure control, and had researched the fuzzy sliding mode variable structure controller design method. This method can not only guarantee the system stability, but also restrain chattering. In the MATLAB for the control system of simulation test, the feasibility of the method is demonstrated.
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Fuzzy Control Strategy for Train Lateral Semi-active Suspension Based on Particle Swarm Optimizationt and rear bogies by using the optimized fuzzy controller reduce by 5.05% and 7.75%, respectively. In comparison with the passive suspension, the values reduce by 13.56% and 15.51%, respectively, which is more significant.
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Numerical Simulation and Linear Active Disturbance Rejection Control of Unstable Heat Conduction Syse an effective actuation on one boundary to get the temperature on the desired position under close-loop control. Finally, the robustness of the proposed controller with respect to external noises and parameter perturbations is also tested.
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Study on General Effectiveness Evaluation Platform for Combat Aircraftzing of test data, recording and replaying of evaluation process, synthesizing of indexes, and generation of evaluation results. As an application instance, EEPCSS is conducted to evaluate the performance of aircrafts in combat simulation. The evaluation result proves that EEPCSS can work effectively in solving practical problems.
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