In this thesis, the development of a 3-axis motion simulator as well as its motion controller, which are used to simulate satellite attitude behavior and then provide laboratory environment for development and testing of satellite instruments, is introduced. This thesis covers the following five research topics on the motion simulator development and related aspects such as permanent magnet synchronous motor (PMSM) drives and Hardware-inthe-loop simulation (HILS) dynamics: (1) Design, development and modeling of a three-axis motion simulator; (2) Development of integral control strategies for the motion simulator; (3) PMSM motion control with initial rotor position uncertainty; (4) IPMSM wide-speed operation; and (5) Preliminary HILS dynam...
Formation flying is an emerging space technology which requires special facilities and methods for t...
Abstract: Cost reduction on system tests with hardware in the loop during qualification phase of the...
Automatic attitude control system test for satellite using inertia wheels mounted on air bearing
In this thesis, the development of a 3-axis motion simulator as well as its motion controller, whic...
AbstractThis paper describes the integration and implementation of a satellite flight simulator base...
In this study, a Hardware-In-the-Loop (HIL) simulator using thrusters is developed to validate the s...
A semi-physical simulation platform for attitude determination and control system is proposed to ver...
This paper deals with the design, manufacturing, and test of a three-axis magnetic field simulator f...
In this paper, a Hardware-In-the-Loop simulator to simulate attitude control of spacecraft using mom...
Kongsberg Defence & Aerospace (KDA) delivers Remote Weapon Stations (RWS) configured on top of a rot...
A small satellite simulator with attitude determination and control was designed and implemented in ...
The development of an attitude control system for a satellite relies heavily on simulation. In the c...
This thesis developed a 3-DOF satellite simulator with an attached 3-DOF manipulator to capture and ...
The study by simulation of different drives architectures can offer valuable information for choosin...
The cost and error of theSatellite Attitude Control System design can be minimize by using ground te...
Formation flying is an emerging space technology which requires special facilities and methods for t...
Abstract: Cost reduction on system tests with hardware in the loop during qualification phase of the...
Automatic attitude control system test for satellite using inertia wheels mounted on air bearing
In this thesis, the development of a 3-axis motion simulator as well as its motion controller, whic...
AbstractThis paper describes the integration and implementation of a satellite flight simulator base...
In this study, a Hardware-In-the-Loop (HIL) simulator using thrusters is developed to validate the s...
A semi-physical simulation platform for attitude determination and control system is proposed to ver...
This paper deals with the design, manufacturing, and test of a three-axis magnetic field simulator f...
In this paper, a Hardware-In-the-Loop simulator to simulate attitude control of spacecraft using mom...
Kongsberg Defence & Aerospace (KDA) delivers Remote Weapon Stations (RWS) configured on top of a rot...
A small satellite simulator with attitude determination and control was designed and implemented in ...
The development of an attitude control system for a satellite relies heavily on simulation. In the c...
This thesis developed a 3-DOF satellite simulator with an attached 3-DOF manipulator to capture and ...
The study by simulation of different drives architectures can offer valuable information for choosin...
The cost and error of theSatellite Attitude Control System design can be minimize by using ground te...
Formation flying is an emerging space technology which requires special facilities and methods for t...
Abstract: Cost reduction on system tests with hardware in the loop during qualification phase of the...
Automatic attitude control system test for satellite using inertia wheels mounted on air bearing