Magnetohydrodynamic Flow Control of a Hypersonic Cruise Vehicle Based on AJAX Concept

Balasubramanian R.; Anandhanarayanan K.; Krishnamurthy R.; Chakraborty Debasis

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Magnetohydrodynamic Flow Control of a Hypersonic Cruise Vehicle Based on AJAX Concept

机译：基于AJAX概念的高超音速巡航车的磁流体动力流控制

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来源
《Journal of Spacecraft and Rockets》 |2016年第4期|759-762|共4页
作者
Balasubramanian R.; Anandhanarayanan K.; Krishnamurthy R.; Chakraborty Debasis;
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作者单位

Def Res & Dev Lab, Directorate Computat Dynam, Hyderabad 500058, Andhra Pradesh, India;

Def Res & Dev Lab, Directorate Computat Dynam, Hyderabad 500058, Andhra Pradesh, India;

Def Res & Dev Lab, Directorate Computat Dynam, Hyderabad 500058, Andhra Pradesh, India;

Def Res & Dev Lab, Directorate Computat Dynam, Hyderabad 500058, Andhra Pradesh, India;

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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
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1. Tracking control for air-breathing hypersonic cruise vehicle based on tangent linearization approach [J] . Cai Guangbin, Duan Guangren, Hu Changhua, Systems Engineering and Electronics, Journal of . 2010,第3期

机译：基于切线线性化方法的呼吸高超音速巡航舰的跟踪控制
2. Tracking control for air-breathing hypersonic cruise vehicle based on tangent linearization approach [J] . Guangbin Cai, Guangren Duan, Changhua Hu, 系统工程与电子技术：英文版 . 2010,第003期

机译：基于切线线性化方法的高空超声速巡航飞行器跟踪控制
3. Tracking control for air-breathing hypersonic cruise vehicle based on tangent linearization approach [J] . Guangbin Cai, Guangren Duan, Changhua Hu, 系统工程与电子技术（英文版） . 2010,第003期

机译：基于切线线性化方法的高空超声速巡航飞行器跟踪控制
4. Hypersonic technologies of atmospheric cruise flight under AJAX Concept [C] . A. Kuranov, A. Korabelnikov AIAA International Space Planes and Hypersonic Systems and Technologies Conference . 2008

机译：AJAX概念下的大气巡航飞行超音速技术
5. Application of parabolized Navier-Stokes numerical analysis methodology in the prediction of flow field and aerodynamic properties of an air-breathing hypersonic cruise vehicle. [D] . Norman, Robert Michael. 1995

机译：抛物线型Navier-Stokes数值分析方法在空气呼吸高超音速巡航飞行器流场和空气动力学特性预测中的应用。
6. Robust Stabilization Control Based on Guardian Maps Theory for a Longitudinal Model of Hypersonic Vehicle [O] . Yanbin Liu, Mengying Liu, Peihua Sun -1

机译：基于Guardian Maps理论的高超音速飞行器纵向模型的鲁棒稳定控制
7. Periodically Cruising Hypersonic Vehicle With Active Cooling: An Optimal-Control Based Design Approach [O] . Wenkai Wang, Zhongxi Hou, Shangqiu Shan, 2019

机译：定期巡航高超声速车辆，具有主动冷却：基于最佳控制的设计方法
8. Control integration concept for hypersonic cruise-turn maneuvers [R] . Raney, David L., Lallman, Frederick J. 1992

机译：高超音速巡航转弯机动的控制一体化概念

Magnetohydrodynamic Flow Control of a Hypersonic Cruise Vehicle Based on AJAX Concept

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