Method for identifying navigational spacecrafts with incomplete information of ranging code
DOI:
https://doi.org/10.15587/1729-4061.2013.16578Keywords:
spacecraft, identification of beacons, navigation, angular orientation, pseudo-random sequenceAbstract
For solving the target tasks spacecrafts require information about their mass centers position and angular positions in a particular terrestrial reference system. Today, satellite navigational equipment is actively used for solving such problems. Existing solution methods are applicable when there is information about the ranging code structure, pseudo-random sequence of each navigation unit. Meanwhile, if the carrier frequency in a wide frequency range is quite difficult to change, the principle of ranging code formation can be changed programmatically (e.g., by changing the order of generator polynomial of a pseudo-random sequence). Taking into account that the GPS and GLONASS navigation groupings are managed by the ministries of Defense of the USA and Russia, such situation may occur. Meanwhile, assuming that the navigation signals transmission will not be terminated, determination of the target device coordinates is possible in case of identification of navigational transmitting spacecraft. The work deals with the problem of navigational unit identification under the changing structure of pseudo-random sequenceReferences
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