![Loading...](https://link.springer.com/static/c4a417b97a76cc2980e3c25e2271af3129e08bbe/images/pdf-preview/spacer.gif)
-
Chapter and Conference Paper
Connectivity Preservation and Collision Avoidance Control for Spacecraft Formation Flying with Bounded Actuation
This paper considers connectivity preservation and collision avoidance controller design for spacecraft formation flying with bounded actuation. A distributed controller with bounded artificial potential funct...
-
Chapter and Conference Paper
Research on Decision Method of Spacecraft Cluster Combination Mode for In-Orbit Service
In order to meet the requirements of in-orbit service, the spacecraft cluster is designed to expand and maintain the functions of cooperative in-orbit spacecraft. In order to improve the autonomy of spacecraft...
-
Chapter and Conference Paper
Orbit Determination Using Combined GPS + Beidou Observations for Low Earth Cubesats: Software Validation in Ground Testbed
Nowadays, satellites in low earth orbit (LEO) can benefit from Global Navigation Satellite System (GNSS), such as Global Positioning System (GPS) of United States, to estimate positions and velocities. As Chin...
-
Chapter and Conference Paper
GPS Receiver Clock Modelling for Kinematic-Based Precise Orbit Determination of Low Earth Orbiters
This paper describes a GPS receiver clock model that can improve the accuracy of kinematic orbit determination for spacecraft in low earth orbit. The receiver clock error is commonly estimated on an epoch-by-e...