Paper Title:
An Architecture Analysis of ADCS for CubeSat: A Recipe for ADCS Design of ICUBE
  Abstract

This research article presents the architecture analysis and design of Attitude determination and control subsystem (ADCS) of the Pico-Satellites especially the CubeSat, developed and launched into the Low Earth orbit (LEO). ADCS is not a stringent requirement for all the CubeSat missions but several missions were specifically designed to test and validate the ADCS. This paper contributes in evaluating the previous ADCS of CubeSat and presents an optimal ADCS design and a recipe for any CubeSat mission and specifically for the upcoming ICUBE of the Institute of Space Technology (IST), Pakistan. The proposed ADCS for ICUBE includes GPS receiver as position sensor while magnetometer as attitude sensor and magnetic coils as the active actuators. The determination will be done by Kalman filter and LQR will be used as a controller.

  Info
Periodical
Chapter
Chapter 24: Semiconductor Materials Manufacturing
Edited by
Wu Fan
Pages
5397-5404
DOI
10.4028/www.scientific.net/AMM.110-116.5397
Citation
N. N. Abbas, H. Xiao, L. Y. Jun, M. Raza, "An Architecture Analysis of ADCS for CubeSat: A Recipe for ADCS Design of ICUBE", Applied Mechanics and Materials, Vols. 110-116, pp. 5397-5404, 2012
Online since
October 2011
Export
Price
$32.00
Share

In order to see related information, you need to Login.

In order to see related information, you need to Login.

Authors: Lei Wang, Yu Shan Zhao, Peng Shi
Chapter 23: Computer-Aided Design, Manufacturing, and Engineering
Abstract:This investigation is concerned with the non-linear multi-in-multi-out tracking control of a spacecraft with Double-gimbaled control moment...
5283
Authors: Lin Zhao, Zhong Hua Su, Yong Hao
Chapter 14: Sensor Technology
Abstract:An attitude determination system has been designed for the geocentric pointing triaxial stabilized satellites which employ a continuously...
1917
Authors: Xiao Han, Xiao Jun Yang, Naqvi Najam Abbas
Chapter 11: Electromechanics and Mechatronics
Abstract:This paper describes an integral scheme of the design and simulation of the Attitude Determination and Control Subsystem (ADCS) of CubeSat....
1582
Authors: W.R. Silva, H.K. Kuga, M.C. Zanardi, R.V. Garcia
Abstract:his work is applied to the dynamics of rotational motion of artificial satellites, that is, itsorientation (attitude) with respect to an...
181