Santa Monica, CA, United States of America

Salma Saeed


Average Co-Inventor Count = 3.0

ph-index = 1

Forward Citations = 11(Granted Patents)


Company Filing History:


Years Active: 2002

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1 patent (USPTO):Explore Patents

Title: Salma Saeed: Innovator in Spacecraft Control Technology

Introduction

Salma Saeed is a prominent inventor based in Santa Monica, CA, who has made significant contributions to the field of spacecraft technology. She holds a patent for a groundbreaking method and apparatus designed to control the attitude and nutation of spinning spacecraft. Her innovative work is crucial for enhancing the stability and maneuverability of spacecraft in orbit.

Latest Patents

Salma Saeed's most notable patent is titled "Minimum fuel attitude and nutation controller for spinning spacecraft." This invention outlines a method that includes measuring the spacecraft's attitude rate about a second axis, generating a rate correction value, and applying torque to rotate the spacecraft along the second axis. The patent emphasizes the importance of precision in controlling spacecraft dynamics, which is essential for successful space missions. Salma holds 1 patent in total.

Career Highlights

Salma Saeed has established herself as a key figure in the aerospace industry through her work at Hughes Electronics Corporation. Her expertise in spacecraft control systems has positioned her as a valuable asset in the development of advanced aerospace technologies.

Collaborations

Throughout her career, Salma has collaborated with notable colleagues, including John W. Smay and John F. Yocum, Jr. These partnerships have contributed to the advancement of innovative solutions in the aerospace sector.

Conclusion

Salma Saeed's contributions to spacecraft technology exemplify her dedication to innovation and excellence. Her patent for a minimum fuel attitude and nutation controller showcases her ability to address complex challenges in aerospace engineering. Salma's work continues to inspire future advancements in the field.

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