Servo design and analysis of thrust vector control of launch vehicle

Author:

Sebastian Arun,Thomas Polly,Alex Sophy

Publisher

IEEE

Cited by 6 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. A hybrid dynamics modeling method for micro-turbine engine thrust vectoring;Journal of Physics: Conference Series;2024-05-01

2. A new propulsion system GUI based control amenable model development for high‐power rockets;Advanced Control for Applications;2024-03-26

3. Design of Isolated Bi-Directional DC-DC Converter for Aerospace;2023 IEEE 2nd International Power Electronics and Application Symposium (PEAS);2023-11-10

4. Multiple Resonant Load Characteristics and Control Strategy of Electro-Hydraulic Actuator for Launch Vehicles;2023 9th International Conference on Fluid Power and Mechatronics (FPM);2023-08-18

5. Friction Estimation of Electromechanical Actuator based Flex Nozzle Control System using Firefly Algorithm;2023 International Conference on Control, Communication and Computing (ICCC);2023-05-19

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