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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
Email:               dai@zess.uni-siegen.de

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

                          Germany

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