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基于INTESIM软件的机翼颤振流固耦合的分析研究
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作者 刘新桥 张群 《进展》 2024年第9期119-122,共4页
本文以航空航天领域多场耦合问题的实际工程应用为背景,基于国内CAE自主软件INTESIM进行流固耦合求解功能模块开发和完善,对航空航天中的典型流固耦合问题进行了数值模拟研究。通过AGARD 445.6案例对基于时域的流固耦合颤振问题进行了... 本文以航空航天领域多场耦合问题的实际工程应用为背景,基于国内CAE自主软件INTESIM进行流固耦合求解功能模块开发和完善,对航空航天中的典型流固耦合问题进行了数值模拟研究。通过AGARD 445.6案例对基于时域的流固耦合颤振问题进行了计算和验证,给出了0.901马赫数在不同无因次速度下的计算结果,得到监测点时间历程曲线的收敛振动、简谐振动和发散振动的三种状态,数值模拟结果与NASA风洞实验结果符合良好,表明了基于INTESIM-GISCI的流固耦合仿真软件在机翼颤振问题的仿真分析中的可靠性。 展开更多
关键词 机翼颤振 流固耦合 耦合控制平台 CSD求解模块 CFD求解模块
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Cross-coupling integral adaptive robust posture control of a pneumatic parallel platform 被引量:1
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作者 左赫 陶国良 《Journal of Central South University》 SCIE EI CAS CSCD 2016年第8期2036-2047,共12页
A pneumatic parallel platform driven by an air cylinder and three circumambient pneumatic muscles was considered. Firstly, a mathematical model of the pneumatic servo system was developed for the MIMO nonlinear model-... A pneumatic parallel platform driven by an air cylinder and three circumambient pneumatic muscles was considered. Firstly, a mathematical model of the pneumatic servo system was developed for the MIMO nonlinear model-based controller designed. The pneumatic muscles were controlled by three proportional position valves, and the air cylinder was controlled by a proportional pressure valve. As the forward kinematics of this structure had no analytical solution, the control strategy should be designed in joint space. A cross-coupling integral adaptive robust controller(CCIARC) which combined cross-coupling control strategy and traditional adaptive robust control(ARC) theory was developed by back-stepping method to accomplish trajectory tracking control of the parallel platform. The cross-coupling part of the controller stabilized the length error in joint space as well as the synchronization error, and the adaptive robust control part attenuated the adverse effects of modelling error and disturbance. The force character of the pneumatic muscles was difficult to model precisely, so the on-line recursive least square estimation(RLSE) method was employed to modify the model compensation. The projector mapping method was used to condition the RLSE algorithm to bound the parameters estimated. An integral feedback part was added to the traditional robust function to reduce the negative influence of the slow time-varying characteristic of pneumatic muscles and enhance the ability of trajectory tracking. The stability of the controller designed was proved through Laypunov's theory. Various contrast controllers were designed to testify the newly designed components of the CCIARC. Extensive experiments were conducted to illustrate the performance of the controller. 展开更多
关键词 servo-pneumatic system pneumatic muscle parallel platform cross coupling adaptive robust control parameter estimation
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