Research on Air Target Attitude Testing Technology
Combining domestic and foreign literature, the technology of flight attitude testing technology was summarized. The research process of this field includes independently inertial measurement unit and inertial navigation system. The previous stage is the test technology only depend on one kind of navigation equipment, such as Gyro, accelerometer or electromagnetic sensors etc, the latter means various combinations of measurement units, on the basis of complementary advantages in performance to improve testing accuracy each other. Based on the testing technology was analyzed and compared, configuration, merit and demerits of multi accelerometer were discussed. The future development of this technology was prospected finally.
Wei Deng and Qi Luo
Z. J. Liang and T. H. Ma, "Research on Air Target Attitude Testing Technology", Applied Mechanics and Materials, Vols. 236-237, pp. 366-369, 2012