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標題: 中高層飛彈導引律設計與分析
Design and Analysis of Medium and Higher-Tier Missile Guidance Law
作者: 李雲皓
Li, Yun-Hao
關鍵字: Ballistic Target;彈道目標;Guidance Law;Control;Performance;導引律;控制;性能
出版社: 電機工程學系所
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The research issue regarding missile guidance law design of a medium and higher-tier anti-ballistic missile to intercept ballistic targets during their early reentry phase has been a major concern in the defense technology. The defense missile possessing two solid rocket stages with both stages based on thrust vector control is used as a reference model for developing the guidance law.
For the guidance law design, the missile trajectory is first shaped by directly controlling its flight path toward the incoming target. When the first-stage rocket burns out, the missile coasts toward to the target with inertia force until the second-stage rocket activates. After the second-stage rocket activates, the missile is guided by proportional navigation guidance law that the angular rates are provided by the ground control center. The modified proportional navigation guidance law, works after the seeker starts, is designed to account the missile's axial acceleration and target acceleration variation. The lateral acceleration command is applied to guide the missile engaging the ballistic target.
The guidance law is developed with the aim to increase the interception performance by incorporating a thrust vector control mechanism to enhance lateral maneuverability and the second stage of the missile fitted with small control fins to stabilize the missile body. The effect of the proposed design is verified via extensive numerical simulation to examine its engagement performance. Miss distance analysis is conducted and characterization of the 3-dimenaional defensible volume is constructed to verify the proposed design.
其他識別: U0005-1708200919581000
Appears in Collections:電機工程學系所

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