Synthesis Guidance Method for Air to Ground Missiles (AGM-ASM) in the Self-guided Phase
摘要
The guidance method for air missiles is very diverse, greatly determining the flexibility of the missile’s trajectory to the target. This article aims to study a method of synthesizing conduction rules for Air to Ground missiles (AGMs-ASM) in the self-guided phase of the goal based on the theory of optimization of the local quality index function or the terminal quality criterion function Letov-Kalman. The research problem is to optimize the motion trajectory and minimize the error at the target meeting point.