The invention discloses a combined orientation and attitude measurement
system and method based on navigation array antennas and MEMS inertial navigation, the
system comprises
satellite navigation array antennas, MEMS inertial navigation, an MEMS inertial navigation attitude resolving module and a combined attitude measurement filter module, one MEMS inertial navigation is integrated in each
satellite navigation array antenna, the
satellite navigation array antennas are connected with the combined attitude measurement filter module, and the MEMS inertial navigation attitude resolving module is connected with the combined attitude measurement filter module. And the MEMS inertial navigation is connected with the combined attitude measurement filter module through the MEMS inertial navigation attitude resolving module. The MEMS inertial navigation is integrated in the
satellite navigation array antenna, on one hand, compared with a traditional combination mode of using
optical fiber inertial navigation or
laser inertial navigation and a
satellite navigation orientation / attitude measurement
system, the system size is effectively reduced, the
system integration degree is improved, and the system cost is reduced; and on the other hand, the orientation and attitude measurement data of the
satellite navigation system and the attitude measurement data of the MEMS
inertial navigation system are fused, so that the orientation and attitude
measurement precision of the
satellite navigation system can be effectively improved, the output frequency of the orientation and attitude data can be improved, and meanwhile, the continuous working capability of the orientation and attitude measurement system can be maintained within a certain time when the satellite navigation
signal is unlocked.