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Application of nonlinear aerodynamic stability characteristics to simplify missile control and guidance systems

机译：应用非线性气动稳定特性简化导弹控制和制导系统

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Curfman, Howard J , Jr;
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年度 1955
页码 1-25
总页数 25
原文格式 PDF
正文语种 eng
中图分类工业技术;
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2. Backstepping-based adaptive predictive optimal control of nonlinear systems with application to missile-target engagement [J] . Sun Jingliang, Liu Chunsheng ISA Transactions . 2018,第期

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3. Nonlinear Controller Synthesis for Single-Input Multiple-Output Systems with Application to Cruise Missile [J] . Amir Nassirharand Journal of aerospace engineering . 2010,第2期

机译：单输入多输出系统的非线性控制器综合及其在巡航导弹中的应用
4. Prediction of the Nonlinear Aerodynamic Characteristics of Tandem- Control and Rolling- Tail Missiles [C] . D. Lesieutre, J. Love, M. Dillenius AIAA Guidance, Navigation, and Control Conference and Exhibit . 2002

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5. Advanced controls of highly nonlinear systems for stability and performance with applications to power plant systems. [D] . Yang, Shizhong. 2010

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6. Modeling and Simulation of Control Actuation System with Fuzzy-PID Logic Controlled Brushless Motor Drives for Missiles Glider Applications [O] . Murali Muniraj, Ramaswamy Arulmozhiyal 2015

机译：模糊PID逻辑控制的无刷电机驱动控制系统的建模与仿真
7. Complexity, Dynamics, Control, and Applications of Nonlinear Systems with Multistability [O] . Viet-Thanh Pham, Sundarapandian Vaidyanathan, Tomasz Kapitaniak 2020

机译：非线性系统的复杂性，动态，控制和应用的非线性系统

Application of nonlinear aerodynamic stability characteristics to simplify missile control and guidance systems

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