What is it about?
This work presents a solution to initial orbit determination using three velocity measurements.
Featured Image
Read the Original
This page is a summary of: Initial Orbit Determination from Three Velocity Vectors, Journal of Guidance Control and Dynamics, April 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g003988.
You can read the full text:
Contributors
The following have contributed to this page
