This study is aimed at addressing the practical challenges of conducting hardware-in-the-
loop simulation (HILS) for a CubeSat attitude determination and control system (ADCS) with …

In most practical applications, the tracking process needs to update the data constantly.
However, outliers may occur frequently in the process of sensors' data collection and …

The attitude determination system is an important subsystem for most satellite missions.
Attitude estimation is often performed using Kalman filters. In particular, for nanosatellites or …

This paper is the second part of a series of studies discussing a novel attitude determination
method for nano-satellites. Our approach is based on the utilization of thermal imaging …

CubeSats have became a common platform for education and technology demonstration. To
overcome restrictions on CubeSat design, the Attitude Determination and Control System …

The highly reliable nanosatellite platforms have broad application prospects in the
construction of satellite Internet. Obtaining accurate attitude information is crucial to enhance …

For a small satellite, the processor onboard the attitude determination and control system
(ADCS) is required to monitor, communicate, and control all the sensors and actuators. In …

This work presents the design and performance analysis of attitude determination algorithms
for CubeSats that fuse rate gyros with a single vector measurement using a sensor set …

This thesis examines CubeSat attitude determination using the Earth's magnetic field (EMF)
vector aiding a low-cost IMU. CubeSats provide relatively cost-effective methods of …

As part of the Bristol PROVE mission, a nano satellite in low Earth orbit will be required to
track a ground based target during a 400 second flyover. This requires agile attitude control …