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Dynamic Modeling and Active Control of a Strap-on Launch Vehicle 被引量:1

Dynamic Modeling and Active Control of a Strap-on Launch Vehicle
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摘要 Dynamic modeling and active control of a strap-on launch vehicle are studied in this paper. In the dynamic modeling, the double-compatible free-interface modal synthesis method is used to establish dynamic model of the system, and its model precision is compared with those of finite element method(FEM), fixedinterface modal synthesis method and free-interface modal synthesis method. In the active control, the swing angle of rocket motor is used as design variable, and the control law design based on the model of mass center motion is adopted to validate the system. Simulation results indicate that the double-compatible model synthesis method can properly approximate the FEM which is used as the benchmark solution, and the model precision of the double-compatible modal synthesis method is obviously higher than those of the fixed-interface and freeinterface modal synthesis methods. Based on the control law design, the deflection of mass center of the launch vehicle is very small. Dynamic modeling and active control of a strap-on launch vehicle are studied in this paper. In the dynamic modeling, the double-compatible free-interface modal synthesis method is used to establish dynamic model of the system, and its model precision is compared with those of finite element method (FEM), fixed- interface modal synthesis method and free-interface modal synthesis method. In the active control, the swing angle of rocket motor is used as design variable, and the control law design based on the model of mass center motion is adopted to validate the system. Simulation results indicate that the double-compatible model synthesis method can properly approximate the FEM which is used as the benchmark solution, and the model precision of the double-compatible modal synthesis method is obviously higher than those of the fixed-interface and free-interface modal synthesis methods. Based on the control law design, the deflection of mass center of the launch vehicle is very small.
出处 《Journal of Shanghai Jiaotong university(Science)》 EI 2016年第4期385-394,共10页 上海交通大学学报(英文版)
基金 the National Natural Science Foundation of China(Nos.11132001,11272202 and 11472171) the Key Scientific Project of Shanghai Municipal Education Commission(No.14ZZ021) the Natural Science Foundation of Shanghai(No.14ZR1421000)
关键词 strap-on launch vehicle dynamic modeling active control 动力学建模 主动控制 运载火箭 模态综合法 动力学模型 自由界面 控制律设计 有限元法
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