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Journal Radioengineering №9 for 2015 г.
Article in number:
Maximum likelihood attitude determination taking into account the effects of global navigation satellite system signals propagation
Keywords:
maximum likelihood
ionospheric scintillation
navigation spacecraft
attitude determination
signal to noise ratio
abnormal error range
Authors:
I.A. Tsikin - Dr. Sc. (Eng.), Professor, Peter The Great St.Petersburg Polytechnic University. E-mail: tsikin@mail.spbstu.ru
E.A. Scherbinina - Assistant, Peter The Great St.Petersburg Polytechnic University. E-mail: lizspbstyle@gmail.com
Abstract:
Maximum likelihood attitude determination on the basis of navigation satellites signals is discussed. Direct maximum likelihood estimation is connected with high DSP computational cost. On the other hand, search of likelihood function maximum can be done under reference phase differences method. Earth-s atmosphere irregularities can lead to rapid fading in received signal power levels. Relations between attitude determination accuracy and a number of satellites is analyzed for different receiving conditions. It has been demonstrated that it is impossible to achieve the same attitude determination accuracy and abnormal error probability range for a low signal to noise ratio as for a high one even thanks to growth in the number of satellites.
Pages: 88-94
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