Alsat-1 First Algerian Low Earth Orbit Observation Microsatellite in Orbit

Author

Mohammed, A. M Si ; Benyettou, M. ; Boudjemai, A. ; Chouraqui, S. ; Hashida, Y. ; Cooksley, J.R. ; Sweeting, M.N.

Author_Institution

Centre Nat. des Techniques Spatiales, Arzew

Volume

2

fYear

0

fDate

0-0 0

Firstpage

2518

Lastpage

2523

Abstract

The attitude determination and control system Alsat-1 uses a Y momentum and Z reaction wheels, 3-axis magnetorquer rods and a single butane gas thruster for orbital maintenance. The magnetorquer rods do momentum maintenance and notation damping for Y/Z wheels, vibration damping and yaw phase control. This paper describes the attitude determination and control system on Alsat-l first Algerian micro satellite in orbit. The attitude determination sensor required, is a magnetometer and sun sensor and the actuator required is a Y/Z wheels and magnetorquer coil. In orbit results is presented

Keywords

artificial satellites; attitude control; damping; phase control; rods (structures); sensors; wheels; 3-axis magnetorquer rods; Algerian low earth orbit observation microsatellite; Alsat-1; Y momentum; Y/Z wheels; Z reaction wheels; actuator; attitude control system; attitude determination sensor; attitude determination system; magnetometer; magnetorquer coil; momentum maintenance and; notation damping; orbital maintenance; single butane gas thruster; sun sensor; vibration damping; yaw phase control; Control systems; Damping; Low earth orbit satellites; Magnetic moments; Magnetic sensors; Magnetometers; Phase control; Position measurement; Vibration control; Wheels;

fLanguage

English

Publisher

ieee

Conference_Titel

Information and Communication Technologies, 2006. ICTTA '06. 2nd

Conference_Location

Damascus

Print_ISBN

0-7803-9521-2

Type

conf

DOI

10.1109/ICTTA.2006.1684803

Filename

1684803