Rancho Palos Verde, CA, United States of America

Sibnath Basuthakur


Average Co-Inventor Count = 2.0

ph-index = 2

Forward Citations = 80(Granted Patents)


Location History:

  • Rancho Palos Verde, CA (US) (1995)
  • Rancho Palos Verdes, CA (US) (1995)

Company Filing History:


Years Active: 1995

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2 patents (USPTO):Explore Patents

Title: The Innovative Contributions of Sibnath Basuthakur

Introduction

Sibnath Basuthakur is a notable inventor based in Rancho Palos Verde, California. He has made significant contributions to the field of aerospace engineering, particularly in spacecraft attitude determination and control systems. With a total of 2 patents, his work has advanced the capabilities of satellite technology.

Latest Patents

One of Basuthakur's latest patents is an on-board three-axes attitude determination and control system. This innovative method and system control the attitude of a spacecraft during its transfer orbit using a stand-alone, three-axes attitude determination and control system. The system employs a set of on-board sensors to define two independent angular measurements, which initially identify the z-axis orientation of the spacecraft after launch vehicle separation. Additionally, a set of three-axis gyros is bias calibrated to measure the transverse rates of the spacecraft. The continuous determination of the spacecraft's three-axis attitude is achieved by integrating the gyro outputs, even when the Earth or Sun is not visible. A state estimator model is also provided to determine the spacecraft's three-axis attitude in the presence of large wobble and nutation.

Another significant patent by Basuthakur focuses on satellite thruster uncertainty estimation in transition mode. This invention addresses the estimation and compensation of fixed, but unknown uncertainties of a thruster to improve satellite attitude estimation and control. The method eliminates the need for nutation damping devices. In this system, a thruster is fired, and an attitude state is estimated using an estimator. A commanded rate change is calculated and modified using a compensating feedforward command, updated by a fixed uncertainty estimator. This modified commanded rate change is then used to incrementally adjust the thruster fire on-time until a predetermined satellite trajectory is achieved.

Career Highlights

Sibnath Basuthakur has had a distinguished career at Hughes Aircraft Company, where he has applied his expertise in aerospace technology. His innovative work has contributed to advancements in satellite systems and spacecraft control.

Collaborations

Throughout his career, Basuthakur has collaborated with notable colleagues, including Loren I Slafer and Bernard C Soriano. These collaborations have further enhanced the impact of his inventions in the aerospace sector.

Conclusion

Sibnath Basuthakur's contributions to aerospace engineering through his patents and work at Hughes Aircraft Company demonstrate his commitment to

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