| 基于PIDA策略的再入飞行控制方法 | |
| Alternative Title | Reentry Flight Control Method Based on PIDA Policy |
李文皓 ; 张珩
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| Source Publication | 系统仿真学报
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| 2011 | |
| Volume | 23Issue:5Pages:969-972 |
| ISSN | 1004-731X |
| Abstract | 阐述了PIDA控制概念及特点,提出了基于PIDA策略的飞行器再入控制方法。以HL-20载人返回飞行器为例,结合PIDA控制的低模型依赖、简单结构、鲁棒性强和动态逆控制的解耦性好的特点,在多舵面组合且偏转受限、气动参数不准、外干扰的情况下进行了控制算法的仿真,充分验证了该方法的有效性。; PIDA control’s conception and characteristics were expatiated,and a control method for aero-craft reentry was proposed based on PIDA policy.Taking HL-20 Aero-craft reentry as an example,and using dynamic inversion control’s uncoupling profit and PIDA control’s low model dependence,simple structure and fast-response characters to design a PIDA combine dynamic inversion controller,the control algorithm was simulated in situation of helms output limit,inaccurate parameters and wind interfere.The simulation conclusion validates the efficiency of the method |
| Keyword | Pida控制 再入控制 动态逆 飞行 |
| Subject Area | 力学 |
| URL | 查看原文 |
| Indexed By | CSCD |
| Language | 中文 |
| CSCD ID | CSCD:4192225 |
| Department | MAM遥科学技术 |
| Citation statistics | |
| Document Type | 期刊论文 |
| Identifier | http://dspace.imech.ac.cn/handle/311007/45148 |
| Collection | 先进制造工艺力学实验室 |
| Corresponding Author | 李文皓 |
| Recommended Citation GB/T 7714 | 李文皓,张珩. 基于PIDA策略的再入飞行控制方法[J]. 系统仿真学报,2011,23(5):969-972. |
| APA | 李文皓,&张珩.(2011).基于PIDA策略的再入飞行控制方法.系统仿真学报,23(5),969-972. |
| MLA | 李文皓,et al."基于PIDA策略的再入飞行控制方法".系统仿真学报 23.5(2011):969-972. |
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| C2011J077.pdf（932KB） | 开放获取 | -- | View Download | |||
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