Daejeon-si, South Korea

Jo Ryeong Yim


 

Average Co-Inventor Count = 8.0

ph-index = 1

Forward Citations = 6(Granted Patents)


Company Filing History:


Years Active: 2013

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1 patent (USPTO):Explore Patents

Title: Jo Ryeong Yim: Innovator in Spacecraft Attitude Control Systems

Introduction

Jo Ryeong Yim is a prominent inventor based in Daejeon-si, South Korea. He has made significant contributions to the field of spacecraft technology, particularly in the area of attitude control systems. His innovative approach enhances the maneuverability and controllability of artificial satellites.

Latest Patents

Jo Ryeong Yim holds a patent for a "Method for improving maneuverability and controllability by simultaneously applying both reaction wheel-based attitude controller and thruster-based attitude controller." This patent describes an advanced attitude control system and method for spacecraft that improves maneuverability by integrating both reaction wheels and thrusters. The system includes a thruster-based attitude controller that manages the firing time of thrusters and a reaction wheel-based attitude controller that regulates the operation of reaction wheels. This dual approach allows for effective correction of attitude maneuverability, especially in cases of partial malfunction of the reaction wheels.

Career Highlights

Jo Ryeong Yim is affiliated with the Korea Aerospace Research Institute, where he applies his expertise in aerospace engineering. His work focuses on developing innovative solutions that enhance the performance of spacecraft. His contributions have been instrumental in advancing the capabilities of artificial satellites.

Collaborations

Jo Ryeong Yim collaborates with notable colleagues, including Hyun Ho Seo and Ki Lyuk Yong. Their combined efforts contribute to the ongoing research and development in aerospace technology.

Conclusion

Jo Ryeong Yim's innovative work in spacecraft attitude control systems exemplifies the importance of advancements in aerospace technology. His patent reflects a significant step forward in enhancing the maneuverability and controllability of artificial satellites.

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