Usinge The qEKF Algorithm for Satellite Attitude Estimation with Two Magnetometer & Sun Sensors
Design and Dynamic Analysis for Vertical and Horizontal Cylindrical Body in Reentry Flight
States' Responsibility to Operate Small Satellites in International Space Law
The Turbulence Model in the Spacecraft by using A Moving Pulsed Ball Model
Hybrid PID-FUZZY Control of Formation Flying of Spacecrafts in order to asteroid Deflection Mission
Modeling and Control of Fuel Sloshing and its Effect on Spacecraft Attitude
Design and implementation of hardware-in-the-loop (HIL) test-bed for spacecraft attitude control
System Design and Analysis of Launch Abort System of Manned Spacecraft in Sub-Orbital Mission
A Nonlinear Attitude Controller for a Launch Abort System of a Manned Spacecraft