Seattle, WA, United States of America

Abhinav G Kamath

This inventor holds 1 USPTO granted patent. Top assignee: University of Washington. Active years: 2026.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Abhinav G Kamath. Retrieved from https://idiyas.com/inventor/abhinav-g-kamath

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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Company Filing History:


Years Active: 2026

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1 patent (USPTO):Explore Patents

Title: Abhinav G Kamath and Aircraft Trajectory Optimization

Introduction

Abhinav G Kamath is an inventor associated with the University of Washington in Seattle, Washington. His patent work addresses the generation of approach and landing trajectories for aircraft with multiple degrees of freedom, subject to operational constraints.

Latest Patents

Kamath is credited with 1 patent: “Generation of Approach and Landing Trajectories with Operational Constraints for Aircraft with Multiple Degrees of Freedom.” The invention describes a system in which a processing device uses instructions stored in memory to receive or determine operational constraints for an aircraft. It then applies an optimization method to produce trajectory data, including temporal state parameters describing the aircraft’s state and control input signals for guiding it. The trajectory data can be transmitted to a flight computer configured to control the aircraft.

Career Highlights

The patent reflects work at the intersection of aircraft guidance, trajectory optimization, and operationally constrained flight planning. By generating trajectory data that accounts for an aircraft’s multiple degrees of freedom, the system is designed to provide a flight computer with information for controlling approach and landing.

Collaborations

Kamath’s listed coworkers include Taewan Kim and Niyousha Rahimi. The patent’s technical focus connects their work to aircraft trajectory planning and flight-control systems.

Conclusion

Abhinav G Kamath’s patent documents an approach to generating operationally constrained approach and landing trajectories, highlighting his contribution to aircraft guidance and control research at the University of Washington.

Profile summary based on public USPTO records.
Data Sources: USPTO Patent Grant XML, Patent Center, EPO & CIPO • Normalized by IDiyas Innovation Graph. Methodology & provenance architecturePlease report any incorrect information to [email protected]
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