方法证据记录
Proportional Navigation
Proportional Navigation (PN) is a guidance law that generates command accelerations proportional to the rate of change of the line-of-sight angle between a pursuer and target. Introduced by Lin-Hsiung Chu in the 1950s, it became the foundation of modern missile guidance systems. PN solves the pursuit-evasion problem by ensuring that the pursuer intercepts a moving target with minimal computational overhead.
源记录
引文逐字复制自方法源记录。这些引文不代表任何层级的验证。
Proportional Navigation Guidance Law
分类方法记录 · process-pipeline / aerospace
- Knox, W. P. (1971). On optimal proportional navigation. IEEE Transactions on Aerospace and Electronic Systems, AES-7(3), 417–426. · URL
- Guelman, M. (1971). Proportional navigation with a maneuvering target. IEEE Transactions on Aerospace and Electronic Systems, AES-8(3), 364–371. · DOI 10.1109/taes.1972.309520
- Lin, C. F., & Tsai, L. L. (2007). Guidance Laws for Missiles. In Modern Control Systems for Unmanned Aerial Vehicles. Butterworth-Heinemann. · URL
精选声明
声明已持久化到证据分类账中，每个声明都有自己的评估。
尚无精选声明
当分类账中没有声明时，此视图不会自行创建声明评估。
相关方法
从方法图中生成，显示为机器建议的关系 — 不推断任何证据声明。