Three-Axis Attitude Estimation Of Satellite Through Only Two-Axis Magnetometer Observations Using LKF Algorithm

Autor: Mehrjardi Mohamad Fakhari, Sanusi Hilmi, Mohd. Ali Mohd. Alauddin

Publikováno v: Metrology and Measurement Systems, Vol 22, Iss 4, Pp 577-590 (2015)

Estimation of satellite three-axis attitude using only one sensor data presents an interesting estimation problem. A flexible and mathematically effective filter for solving the satellite three-axis attitude estimation problem using two-axis magnetom

Externí odkaz: https://doaj.org/article/77f1b9d1e8054b94a9b292db8774f70e

Lateral Thinking through Black Box Experiment among Engineering Students

Autor: Arsad, Norhana, Sanusi, Hilmi, Majid, Rosadah Abd, Ali, Manisah Mohd, Husain, Hafizah

Publikováno v: In Procedia - Social and Behavioral Sciences 17 October 2012 60:14-20

Expert Idea on Liquid Limit and Plastic Limit Estimation with Soil Resistivity Profile

Autor: CHİK, Zamri, Islam, S.M. Taohidul, SANUSİ, Hilmi, MUSTAFA, Mohd. Marzuki

Publikováno v: Volume: 2, Issue: 4 19-23
TOJSAT

This paper presents the idea on determination of liquid limit and plastic limit with soil electrical resistivity in geotechnical investigations. Depending on the moisture contents, the soil behavior is revealed as solid, semisolid, plastic and liquid

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=tubitakulakb::c5fd9d3b72df79e447735e167be2a4f8
https://dergipark.org.tr/tr/pub/tojsat/issue/22667/242084

Epoch Time Assisted Orbit Determination for Near Equatorial Low Earth Orbiting Satellites

Autor: Sanusi, Hilmi, J.du-Plessis, Jan

Publikováno v: AIAA/USU Conference on Small Satellites

GPS (Global Position Systems) have been widely used on microsatellites to provide the ephemerid but availability of the GPS measurement cannot be guaranteed. Orbit estimators based on celestial objects from available attitude sensors with a fraction

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=od______1459::fd24daf688a828af4d6f73d866b414cd
http://digitalcommons.usu.edu/smallsat/2002/all2002/23

Developing a proposed satellite reaction wheel model with current mode control.

Autor: Mehrjardi, Mohamad Fakhari, Sanusi, Hilmi, Ali, Mohd. Alauddin Mohd.

Publikováno v: 2015 2nd National Foundation for Science & Technology Development Conference on Information & Computer Science (NICS); 2015, p410-413, 4p