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Performance Comparisons between Command to Line-of-Sight Guidance Law and Proportional Navigation Guidance Law in Short Range Surface-to-Air Missile

机译：在短程面对空中导弹中指挥对视线指导法的绩效比较和比例导航指导法

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1. Post-flight Analysis and Design Improvement in Command Guidance System for a Short-range Surface-to-air Missile System [J] . Ajit B. Chaudhary, Anil Kumar D. Uttarkar, Prashant Vora, Defence Science Journal . 2005,第3期

机译：短程地空导弹系统指挥制导系统的飞行后分析和设计改进
2. Post-flight Analysis and Design Improvement in Command Guidance System for a Short-range Surface-to-air Missile System [J] . Ajit B. Chaudhary, Anil Kumar D. Uttarkar, Prashant Vora, Defence science journal . 2005,第3期

机译：短程地空导弹系统指挥制导系统的飞行后分析及设计改进
3. An Expanded Two-Dimensional Proportional-Derivative Command to Line-of-Sight Guidance Law [J] . Borislav G. Penev Gyroscopy and navigation . 2018,第4期

机译：视线制导律的二维二维比例微分指令
4. Fuzzy guidance law for surface-to-air missile in the command control systems [C] . Pham Trung-Dung, Tran Qui, Vu Duc-Vuong 2012 International Conference on Control, Automation and Information Sciences. . 2012

机译：指挥控制系统中地空导弹的模糊制导律
5. Guidance laws for a short-range attack missile. [D] . Muzumdar, Dinesh Vasant. 1995

机译：短程攻击导弹的制导法。
6. Terminal attack trajectories of peregrine falcons are described by the proportional navigation guidance law of missiles [O] . Caroline H. Brighton, Adrian L. R. Thomas, Graham K. Taylor 2017

机译：游击猎鹰的终末攻击轨迹由导弹的比例导航制导定律描述
7. Performance Comparison between True Proportional Navigation Guidance Law and Pure Proportional Navigation Guidance Law [O] . 2007

机译：真正比例导航指导法与纯比例导航指导法之间的性能比较

Performance Comparisons between Command to Line-of-Sight Guidance Law and Proportional Navigation Guidance Law in Short Range Surface-to-Air Missile

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