Yazan Chihabi
Papers
1
Total Citations
9
H-Index
1
About
Yazan Chihabi is a researcher specializing in astrodynamics and spacecraft relative motion, with a focus on developing analytical solutions for complex orbital environments. His most cited work, "Linear time-varying state transition matrix for spacecraft relative dynamics on highly elliptical orbits" (2022, 9 citations), addresses a critical challenge in space mission design: accurately modeling the relative motion of spacecraft in highly elliptical orbits without relying on computationally intensive numerical integration. By deriving a closed-form, linear time-varying state transition matrix, Chihabi’s contribution enables efficient and precise trajectory planning for formation flying, rendezvous, and proximity operations in non-circular orbits—a key enabler for missions involving Earth observation, debris removal, or deep-space exploration. This work bridges a gap between simplified circular-orbit models and full numerical simulations, offering practical tools for mission analysts. While his citation count is modest, the novelty and utility of his approach in a niche but vital area of astrodynamics signal a promising trajectory. Chihabi’s research exemplifies how elegant mathematical formulations can streamline spacecraft operations, making him a rising voice in the field of orbital mechanics.
Research Focus
Key Achievements
Top Papers
- 1