An integrated guidance and control approach in three-dimensional space for hypersonic missile constrained by impact angles

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• 作者：Xiaodong Liu ; ^{k.start@163.com} ; Wanwei Huang ^{wwhuang@163.com} ; Lifu Du ^{dulifu0328@163.com}
• 关键词：Dynamic surface control ; Dynamic inversion control ; Integrated guidance and control ; Nonlinear control ; Robust control
• 刊名：ISA Transactions
• 出版年：2017
• 出版时间：January 2017
• 年：2017
• 卷：66
• 期：Complete
• 页码：164-175
• 全文大小：1086 K
• 卷排序：66

文摘

We explore the 3D-IGC design method for hypersonic missile which is lacking currently. A new 3D-IGC design model with more generality is deduced for hypersonic missile. A robust dynamic inversion controller is proposed to enhance the robustness of nonlinear system. A robust 3D-IGC law is proposed for hypersonic missile along with the proof of stability. The proposed 3D-IGC modeling and design method has good generality and extensionality.