Control of the intake shock-position in the test rig for ramjet engine-Reference-Cited by-同舟云学术

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Control of the intake shock-position in the test rig for ramjet engine

Published:1997-07-06 Issue: Volume: Page:
ISSN:
Container-title:33rd Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Ohshima Takao¹,Kanabe Katsuhiro¹,Kimura Hideo¹,Fujiwara Kenji¹,Suzuki Kazuo²,Yanagi Ryoji²,Ohshima Takao¹,Kanabe Katsuhiro¹,Kimura Hideo¹,Fujiwara Kenji¹,Suzuki Kazuo²,Yanagi Ryoji²

Affiliation:

1. Kawasaki Heavy Industries, Ltd., Akashi, Japan

2. National Aerospace Lab., Chofu, Japan

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-2885

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Robust control design of an air‐breathing engine for a supersonic vehicle using backstepping and UKF;Asian Journal of Control;2017-03-06

2. Nonlinear Control of an Air-breathing Engine: A Practical Approach Using Dynamic Inversion and EKF;AIAA Guidance, Navigation, and Control Conference;2010-06-26

3. Modeling, Dynamic Simulation, and Controller Design for an Air-Breathing Combustion System;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05

4. Experimental Study on the Control of the Supersonic Axisymmetric Intake under the Acceleration/Deceleration Conditions;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2003

5. Experimental approach to the HYPR Mach 5 ramjet propulsion system;34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;1998-07-13

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