| 摘要: |
| 考虑运载火箭飞行过程中的弹性振动特性，对运载火箭进行全量动力学建模以及控制器设计。首先将运载火箭考虑为一维梁模型并建立全量动力学模型，分别引入自适应滤波姿态控制算法和H2范数鲁棒增益调度控制算法设计控制器。仿真结果表明：在考虑舵机非线性情况下两种控制方法均能够满足精度要求，在具有较大外部扰动情况下，鲁棒增益调度控制算法相较于自适应滤波算法具有较强的鲁棒性。 |
| 关键词: 运载火箭 刚弹耦合 自适应滤波 H2范数鲁棒增益调度控制 |
| DOI： |
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| 基金项目: |
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| The Modeling and Controller Design for Aeroelastic Rocket Launcher |
| WEI Chang-zhu,JU Xiao-zhe,ZHANG Liang,CUI Nai-gang |
| (Department of Aeronautics, Harbin Institude of Technology) |
| Abstract: |
| Modeling and controller designing for rocket launcher was carried out considering its elastic characteristic during the flight Firstly a full variable dynamic model for the launcher was established based on the one dimensional beam, An adaptive filtering attitude controller and a H2norm robust gain-scheduled controller were introduced Simulation results show that the both controllers perform well without neglecting actuators’ nonlinear characteristic, and the latter is of more robustness against large outer disturbance |
| Key words: Elastic vibration Full variable dynamic model Rigid-elastic coupling Adaptive filtering H2norm Robust gain-scheduled control |