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Electromechanical Actuator Control of Gliding Guided Projectile
Details
As the key actuator of gliding extended range guided projectile, the performance of EMA (Electromechanical Actuator) directly affects its flight quality and strike accuracy. At present, the development mainstream of EMA system is to use BLDCM (Brushless Direct Current Motor) and combine with intelligent control algorithm to realize the fast speed, high accuracy and stable control, which gradually presents the trend of precision, intelligence, universality, modularization and low cost. Taking the EMA of guided projectile as research object, this paper carries out a series of researches around the mathematical modeling, intelligent control algorithms, software and hardware design, motion performance testing and verification, anti-high overload structure optimization and experimental verification.
Autorentext
Dr. Hongqiao Yin is a lecturer at the School of Automation, Jiangsu University of Science and Technology. He obtained his Bachelor's degree in Measurement and Control Technology and Instruments from Shandong University of Technology in 2016, followed by a Master's degree in Control Engineering from Nanjing University of Science and Technology.
Weitere Informationen
- Allgemeine Informationen
- GTIN 09786208848095
- Genre Electrical Engineering
- Sprache Englisch
- Anzahl Seiten 280
- Herausgeber Scholars' Press
- Größe H220mm x B150mm x T17mm
- Jahr 2025
- EAN 9786208848095
- Format Kartonierter Einband
- ISBN 978-620-8-84809-5
- Veröffentlichung 17.06.2025
- Titel Electromechanical Actuator Control of Gliding Guided Projectile
- Autor Hongqiao Yin
- Untertitel Research on Electromechanical Actuator Control and Anti-high Overload of Gliding Extended Range Guided Projectile
- Gewicht 435g