| Citation: | XIAN Yong, REN Leliang, YANG Zicheng, et al. Terrain match aided navigation method of hypersonic glide vehicle[J]. Journal of Beijing University of Aeronautics and Astronautics, 2020, 46(4): 691-702. doi: 10.13700/j.bh.1001-5965.2019.0310(in Chinese)
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The height of the hypersonic vehicle gliding flight is over 30 km, so the atmosphere is extremely thin and the traditional terrain match aided navigation with barometric altimeter cannot work properly. In order to improve the accuracy of terrain match, on the basis of analyzing the insensitivity of the matching algorithm to the terrain constant value error, the scheme of using inertial system to solve absolute height is demonstrated in detail, and the scheme that simplifies the short-time gliding trajectory to equal high flight is compared and analyzed. Based on the strap-down inertial navigation system (SINS) error model, the analytic model of the short-time stability of the inertial system is established by the height channel block diagram and Laplace transformation. In addition, the numerical simulation environment is established with CAV-H as study object. The simulation results show that the analytical model has high accuracy and the scheme that the absolute height is solved by SINS can meet the accuracy requirements of terrain match aided navigation system, which is better than the accuracy of the normal operation of the barometric altimeter.
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