Space subsystems design: (navigation, control, structure and…)
Development of MIL and PIL testbed for Student Microsatellite Attitude Control Subsystem

Niki Sajjad; Mehran Mirshams; Shahrokh Jaliian

Volume 13, Issue 3 , September 2020, , Pages 51-62

Abstract
  This paper presents design, analysis and performance verification test of student microsatellite Attitude Determination and Control Subsystem (ADCS) . ADCS design and implementation procedure contains several various steps. There are four main test levels during simulation called “Model-in-the-Loop”, ...  Read More

Modeling and Simulating the Earth’s Magnetic Field Utilizing the 10th Generation of IGRF and Comparison the Linear and Nonlinear Transformation in order to Use in Satellite Attitude Control

M. Navabi; N. Nasiri

Volume 3, Issue 2 , January 2011, , Pages 45-52

Abstract
  Since last decades utilizing satellites in low earth orbits have had increasing tendency. These satellites experience the earth magnetic field due to their low altitude to the earth. The Earth magnetic intensity can be used in order to control the attitude of spacecraft utilizing the interaction between ...  Read More

Designing, Testing and Evaluation of Single Gimbal Control Moment Gyro for Microsatellite

A. R. Aghalari; A. Kalhor; S. M. Dehghan; A. Abedian

Volume 2, Issue 1 , April 2009, , Pages 13-23

Abstract
  In this paper, a designing procedure of Single Gimbal Control Moment Gyro (SGCMG) for performing an agile slew maneuver in a microsatellite is described, then a prototype is fabricated and finally the test results are presented. The design of actuator mechanism is based on simplicity, direction of produced ...  Read More