本文是对现代空对空导弹制导与控制技术的评述,所涉及的方面包括目标状态估计、先进制导规律、倾斜转弯自动驾驶仪。对非线性滤波、自适应滤波、现代控制、自适应控制、双模控制、微分博奕理论,以及现代控制设计技术应用于空对空导弹问题的假设、限制与收效都将予以讨论。 This article is a review of the guidance and control technology of modern air-to-air missiles. The aspects involved include the estimation of target states, advanced guidance laws, and steep-turning autopilots. The assumptions, limitations and benefits of non-linear filtering, adaptive filtering, modern control, adaptive control, dual-mode control, differential game theory, and modern control design techniques for airspace-to-air missiles are all discussed.