OALib Journal期刊
ISSN: 2333-9721
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基于滑模方法的自适应一体化导引与控制律设计
, PP. 191-198
Keywords: 飞行器控制、导航技术,导引控制一体化,寻的导弹,滑模,自适应
Abstract:
?研究了寻的导弹的导引控制一体化设计问题。建立了俯仰通道的一体化导引与控制系统模型研究了寻的导弹的导引控制一体化设计问题。建立了俯仰通道的一体化导引与控制系统模型,并利用非线性状态变换将模型转化为标准形式;为处理系统中存在的非匹配未知有界不确定性,采用滑模控制方法设计了自适应的非线性一体化导引与控制律,该反馈控制律不但可以保证导弹精确命中目标,而且能保证导弹自身姿态的稳定性。导弹的六自由度非线性数值仿真结果验证了所提的导引控制一体化设计策略的正确性和可行性。
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