Matlab Toolbox zurück zurück

MATLAB toolbox for attitude determination of a non-dedicated GPS multi-antenna system.


By inputting the RINEX observation and navigation files from at least 3 antenna/receiver pairs, the attitude parameters, namely yaw, roll and pitch, are computed from the C/A code derived baselines. If the resolved ambiguities are available, carrier phases can also be used for attitude determination. Two techniques are employed to calculate the attitude parameters: (1) direct attitude computation technique for the case that the baseline information is not known. (2) least-squares attitude estimation for the case that the baselines between antennas are obtained in advance. Last modified: 30.Sept.2008


Questions, comments and corrections are welcomed and can be sent to:

Zhen Dai

Phone:             +49 (0)271 740 2718

Fax:                  +49 (0)271 740 4018

Address:         Center for Sensor Systems (ZESS)

                          University of Siegen

                          Paul-Bonatz Str. 9-11

                          D-57068 Siegen




ZESS Webmaster Team 2018 Disclaimer