Damage-mitigating control of a reusable rocket engine

Author:

Ray Asok1,Dai Xiaowen1,Wu Min-Kuang1,Carpino Marc1,Lorenzo Carl F.2

Affiliation:

1. Pennsylvania State University, University Park, Pennsylvania 16802

2. NASA Lewis Research Center, Cleveland, Ohio 44135

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Reference23 articles.

Cited by 21 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. Throttling simulation and control of liquid oxygen/liquid methane rocket engine pressurized by the electric pump;Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering;2024-01-05

2. Analysis of damage characteristics of an aeroelastic model for air-breathing hypersonic vehicles;Aircraft Engineering and Aerospace Technology;2022-06-10

3. Failure Criteria and Their Application Combined with System Structure Defects;Advances in Astronautics Science and Technology;2022-04-04

4. A Reinforcement Learning Approach for Transient Control of Liquid Rocket Engines;IEEE Transactions on Aerospace and Electronic Systems;2021-10

5. Index allocation for a reusable LOX/CH4 rocket engine;Chinese Journal of Aeronautics;2021-02

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