Use of new developments of attitude control sensors for the micro satellite Flying Laptop

AIAA 57th International Astronautical Congress, IAC 2006

Volumn 6, Issue , 2006, Pages 3562-3573

  Waidmann, Matthias ^a   Waidmann, Christian ^a   Saile, Dominik ^a   Grillmayer, Georg ^a   Wolter, Viola ^b  

^a UNIVERSITY OF STUTTGART   (Germany)

^b Steinbeis Transferzentrum Raumfahrt   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

ATTITUDE CONTROL; GLOBAL POSITIONING SYSTEM; MAGNETOMETERS; OSCILLATORS (ELECTRONIC); SATELLITES; TORQUE MEASUREMENT;

ATTITUDE SENSORS; ELECTRONIC BOARDS; MECHANICAL HOUSINGS; MICRO SATELLITES;

MICROSENSORS;

EID: 40749149574     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.iac-06-b5.6.18     Document Type: Conference Paper

References (5)

1. Grillmayer, G., Falke, A. and Roeser, H.P., "Technology Demonstration with the Micro-Satellite Flying Laptop", Selected Proceedings of the 5th IAA Symposium on Small Satellites for Earth Observation, Berlin, Germany, 4-8 Apr. 2005, pp. 419-427.
2. Grillmayer, G., Hirth, M., Huber, F., Wolter, V., "Development of an FPGA Based Attitude Control System for a Micro-Satellite", AIAA-2006-6522, AIAA/AAS Astrodynamics Specialist Conference, Keystone, CO, USA, 21-24 Aug. 2006.
3. Litef GmbH, "Specification of the Litef C-FORS fiber-optic gyroscope", 144410-0000-312, Rev. B, 2005.
4. Technical University of Denmark, "micro-Advanced Stellar Compass User's Manual", IRS-DTU-MA-3001, Issue 1.1, 2005.
5. Zarm-Technik GmbH, "Magnetometer Manual (MM)", IRS-ZAR-MAG-MM-01-0001, Issue 1, 2006.