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基于PIDA策略的再入飞行控制方法
Alternative TitleReentry Flight Control Method Based on PIDA Policy
李文皓; 张珩
Source Publication系统仿真学报
2011
Volume23Issue:5Pages:969-972
ISSN1004-731X
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
KeywordPida控制 再入控制 动态逆 飞行
Subject Area力学
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Indexed ByCSCD
Language中文
CSCD IDCSCD:4192225
DepartmentMAM遥科学技术
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Document Type期刊论文
Identifierhttp://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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