Franquiz, Francisco J., "Attitude Determination & Control System Design and Implementation for a 6U CubeSat Proximity Operations Mission" (2015). Dissertations and Theses. 266. This …

CubeSat’s ADCS through computer simulations, such as in MATLAB, and to ultimately determine necessary actuators to control the spacecraft within a calculated pointing error budget. This …

Last year’s CubeSat-ADCs team has already selected the control method and algorithm designs. For the control of the CubeSat, there are three phases after launch: de-tumbling, initial attitude …

How well does it need to hold an attitude? This chapter: Defines the Attitude Determination, Control, Navigation, and Sensing (ADCS) system; Distinguishes the responsibilities; Describes …

Feb 13, 2020 · The aim of the project is to study and model the attitude of a 6U CubeSat in Earth orbit pointing an inertial target (star), implement control algorithms using given sensors and …

attitude determination is calculated using quaternion algorithm and implemented using PID controller by linearizing the system model. In this project, the proposed control approach is …

This work aims at aptly recognizing the internal dynamics of a CubeSat and simulates the performance in the presence of disturbance torques. The simulation performed here makes …

In this article, Matlab-Simulink is applied to construct dynamic mathematical models including the CubeSat body. (kinematics, dynamics) module, the three-axis actuator module (BLDCM, …

This thesis describes the complete attitude and formation control design for the MotherCube formation flight technology demonstration mission in LEO. A model of the spacecraft’s sensors …

This thesis is focused on the study, design and simulation of an Attitude Control System for a 1U CubeSat. The simulations and their proper validation are carried out with MATLAB/Simulink. It …