Due to increased human activity in the last two decades, the near-earth space is becoming congested from functional/non-functional satellites and space debris.
The objective of the project is to develop optimal control schemes for controling launch vehicle trajectory
This project focuses on developing a Precise Orbit Determination algorithm for LEO satellites
The objective of the project is to develop an accurate GNSS interference source tracking and identification mechanism
Global and Regional Navigation Satellite Systems are well known for their primary purpose i.
There are more than 20000 man-made objects of more than 10 cm in size floating around in near-earth space which pose collision threats to functional satellites.