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151.
为减小导弹电液伺服机构滑模变结构跟踪控制中的抖振,研究了一种模糊滑模变结构控制(FS-MVSC)方法。给出了模糊滑模控制器的构成,以及模糊化、模糊规则与推理、反模糊化处理的方法。在保持系统对参数变化和外干扰不确定强鲁棒性的同时,可使系统具有较优的动态响应和稳态控制精度。仿真结果表明,该控制方案有效。 相似文献
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Icing is one of the crucial factors that could pose great threat to flight safety,and thus research on stability and stability region of aircraft safety under icing conditions is significant for control and flight.Nonlinear dynamical equations and models of aerodynamic coefficients of an air craft are set up in this paper to study the stability and stability region of the aircraft under an icing condition.Firstly,the equilibrium points of the iced aircraft system are calculated and analyzed based on the theory of differential equation stability.Secondly,according to the correlation theory about equilibrium points and the stability region,this paper estimates the multidimensional stability region of the aircraft,based on which the stability regions before and after icing are compared.Finally,the results are confirmed by the time history analysis.The results can give a reference for stability analysis and envelope protection of the nonlinear system of an iced aircraft. 相似文献
155.
研究了飞机附件软时限的设定和管理方法,该方法可将附件的故障发生机率和运行风险控制在可接受水平,减少航空公司因机务原因的延误,提高飞机可利用率。 相似文献
156.
Leakage due to wear is one of the main failure modes of aero-hydraulic spool valves. This paper established a practical coupling wear model for aero-hydraulic spool valves based on dynamic system modelling theory. Firstly, the experiment for wear mechanism verification proved that adhesive wear and abrasive wear did coexist during the working process of spool valves. Sec-ondly coupling behavior of each wear mechanism was characterized by analyzing actual time-variation of model parameters during wear evolution process. Meanwhile, Archard model and three-body abrasive wear model were utilized for adhesive wear and abrasive wear, respectively. Furthermore, their coupling wear model was established by calculating the actual wear volume. Finally, from the result of formal test, all the required parameters for our model were obtained. The relative error between model prediction and data of pre-test was also presented to verify the accuracy of model, which demonstrated that our model was useful for providing accurate prediction of spool valve’s wear life. 相似文献
157.
将情境式设问与授课内容导入交互结合的模式融入精读课堂教学,能有效提高教学效果和效率。本文以《21世纪大学英语》(读写教程第三册)Unit3,Text A,The Sense of Wonder为例,具体分析了情境式设问与课文内容导入相结合的课堂设计方案和应用策略。 相似文献
158.
陶涛 《中国民航飞行学院学报》2012,(6):13-16
民航英语是专门用途英语的一个分支,民航英语翻译属于应用翻译范畴,应坚持目的性原则。本文从词汇、句法及文体三个层面,分析了民航翻译工作的特点和难点,并结合翻译实践,探讨了翻译方法和翻译策略。 相似文献
159.
蔡忠良 《长沙航空职业技术学院学报》2013,(4):18-21
寻求何种途径培养具有较强实践能力的应用型人才,成为各个高校FI语教学研究和改革的重点。文章分析了学生日语实践能力培养体系构建的原则,提出了地方高校日语学生实践能力的培养策略,即重视具有较强的双师型日语实践教学教育团队的培养.构建以能力培养为主线的日语实践教学内容体系,建立多元化的日语实践能力评价机制以及整合校内实践资源并积极稳妥开拓校外日语实践基地等。 相似文献
160.
Singularity analysis for single gimbal control moment gyroscope system using space expansion method 总被引:2,自引:2,他引:0
Control Moment Gyroscope (CMG) is an effective candidate for agile satellites and large spacecraft attitude control because of its powerful torque amplification capability. The most serious situation, however, in using CMG is the inherent geometric singularity problem, where there’s no torque output along a particular direction. Space expansion method has been proposed in this work for the singularity analysis. Based on inverse mapping transformation, an expanded Jacobian matrix which is a full rank square matrix is obtained. The singular angle sets of the 3-parallel cluster and pyramid cluster are distinguished using space expansion method. An effective hybrid steering strategy, able to deal with the elliptic singularity, is further proposed. Simulation results demonstrate the excellent performance of the proposed steering logic compared to the generalized singular robust logic and pseudo inverse logic in terms of energy consumption and torque error. 相似文献