PD control and the unwinding effect in quaternion parameterized attitude control
The unit quaternion is popular in the representation and control of rigid body attitude
systems. However, it is known that two equilibrium points in the unit quaternion attitude …
systems. However, it is known that two equilibrium points in the unit quaternion attitude …
Rotation vector and directional cosine matrix in problems of satellite attitude control
YV Kim - … Journal of Intelligent Systems Technologies and …, 2022 - inderscienceonline.com
For many years, three rotation angles of moving vehicles: roll, pitch, and yaw have been
used for attitude determination and control. However, in the last years due to appearance of …
used for attitude determination and control. However, in the last years due to appearance of …
[PDF][PDF] Asymptotic stability of quaternion-based attitude control system with saturation function
H Septanto, D Suprijanto - International Journal of Electrical and …, 2017 - academia.edu
In the design of attitude control, rotational motion of the spacecraft is usually considered as a
rotation of rigid body. Rotation matrix parameterization using quaternion can represent …
rotation of rigid body. Rotation matrix parameterization using quaternion can represent …
Simulasi PMDC Menggunakan PID dengan Tuning Ziegler Nichols dan Algoritma Genetika
DWA Ningtias, S Syafrudi - Jurnal Teknik Elektro dan …, 2022 - jurnal.unmuhjember.ac.id
Abstract Kecepatan motor DC Permanen Magnet (PMDC) dapat dikontrol menggunakan
Proportional Integral Derivative (PID) kontroler. PID merupakan sebuah pengontrol yang …
Proportional Integral Derivative (PID) kontroler. PID merupakan sebuah pengontrol yang …
Attitude consensus using quaternion-based controller composing augmented dynamic
H Septanto, RT Bambang… - 2014 IEEE 4th …, 2014 - ieeexplore.ieee.org
Nonlinearity of dynamics and kinematics, difficulty in stability guarantee and unwinding
phenomenon problem make quaternion-based attitude control system design is a non trivial …
phenomenon problem make quaternion-based attitude control system design is a non trivial …
Model Development and Attitude Control for pico-satellite UWE-4
S Dadhich - 2015 - diva-portal.org
The beginning of space age was marked by the launch of Sputnik1 on October 4, 1957. This
event started a space race between the Soviet Union and the USA which lasted for almost …
event started a space race between the Soviet Union and the USA which lasted for almost …