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371.
A fuzzy robust nonlinear controller for hydraulic rotary actuators in flight motion simulators is proposed. Compared with other three-order models of hydraulic rotary actuators, the proposed controller based on first-order nonlinear model is more easily applied in practice, whose control law is relatively simple. It not only does not need high-order derivative of desired command,but also does not require the feedback signals of velocity, acceleration and jerk of hydraulic rotary actuators. Another advantage is that it does not rely on any information of friction, inertia force and external disturbing force/torque, which are always difficult to resolve in flight motion simulators. Due to the special composite vane seals of rectangular cross-section and goalpost shape used in hydraulic rotary actuators, the leakage model is more complicated than that of traditional linear hydraulic cylinders. Adaptive multi-input single-output(MISO) fuzzy compensators are introduced to estimate nonlinear uncertain functions about leakage and bulk modulus. Meanwhile, the decomposition of the uncertainties is used to reduce the total number of fuzzy rules. Different from other adaptive fuzzy compensators, a discontinuous projection mapping is employed to guarantee the estimation process to be bounded. Furthermore, with a sufficient number of fuzzy rules, the controller theoretically can guarantee asymptotic tracking performance in the presence of the above uncertainties, which is very important for high-accuracy tracking control of flight motion simulators.Comparative experimental results demonstrate the effectiveness of the proposed algorithm, which can guarantee transient performance and better final accurate tracking in the presence of uncertain nonlinearities and parametric uncertainties. 相似文献
372.
Space robot is assembled and tested in gravity environment, and completes on-orbit service(OOS) in microgravity environment. The kinematic and dynamic characteristic of the robot will change with the variations of gravity in different working condition. Fully considering the change of kinematic and dynamic models caused by the change of gravity environment, a fuzzy adaptive robust control(FARC) strategy which is adaptive to these model variations is put forward for trajectory tracking control of space robot. A fuzzy algorithm is employed to approximate the nonlinear uncertainties in the model, adaptive laws of the parameters are constructed, and the approximation error is compensated by using a robust control algorithm. The stability of the control system is guaranteed based on the Lyapunov theory and the trajectory tracking control simulation is performed. The simulation results are compared with the proportional plus derivative(PD) controller, and the effectiveness to achieve better trajectory tracking performance under different gravity environment without changing the control parameters and the advantage of the proposed controller are verified. 相似文献
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宾馆火灾风险评估初探 总被引:1,自引:0,他引:1
黄涛 《沈阳航空工业学院学报》2007,24(1):75-77
在分析宾馆火灾发生原因的基础上,建立了宾馆火灾危险性、火灾损失评估因素集,并运用模糊评价法对宾馆的火灾安全进行风险性和损失评价,通过评价得出建筑物所属的安全等级,从而为宾馆实施安全管理提供方向和依据。该方法的建立可用于保险公司对投保建筑的鉴别与筛选,同时也可使管理者根据该评估方法及时采取防火安全措施,以降低火灾危险性,减少火灾损失。 相似文献
375.
采用形状函数法描述变形镜校正时的曲面,从适配误差、Strehl比、加工工艺性三个方面比较了4种不同单元排列方式的微变形镜。结果表明方形排列的微变形镜设计简单,需驱动电压较低,但波前校正性能较差;圆形微变形镜性能最优,但设计复杂,需驱动电压最高。 相似文献
376.
多模型方法在飞控系统故障重构控制中的应用 总被引:2,自引:0,他引:2
基于多模态控制方法,将多模型选择模态的方法用于飞机发生故障时的重构控制:设计多个不同状态的模型及其控制器,模型采用固定模型和自适应模型,相应控制器按模型匹配方法设计,理想模型依飞行品质要求设计。依据转换标准判断当前飞机状态与哪一个模型最接近并转换到相应控制器上。自适应模型及其控制器是采用基于梯度的参数调节方法设计和实现的。最后以某机为例进行了仿真验证,结果表明该方法是有效的。 相似文献
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