Abstract
Aiming at the problem of relative information acquisition in air-to-air missile cooperative navigation, a method of cooperative navigation based on GNSS is proposed. Based on the master-slave structure, the relative navigation state equation between the follower and the leader is designed, and the measurement equation based on double difference pseudo range and pseudo range rate of satellite navigation is derived. The relative deviation is estimated by Kalman filter, and finally the algorithm is proved by simulation. The simulation results show that the designed method can obtain high-precision deviation estimation; the estimation error of relative position is less than 5 m, the estimation error of relative velocity is less than 0.2 m/s, and the deviation of relative attitude estimation error is less than 4′. This method solves the problem of obtaining the error information of relative position, relative velocity and relative attitude of multiple missiles, which lays a foundation for realizing the cooperative detection of multiple missiles.
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Cheng, H., Lu, H. (2023). Research on Air-to-Air Missile Cooperative Navigation Technology Based on GNSS. In: Yan, L., Duan, H., Deng, Y. (eds) Advances in Guidance, Navigation and Control. ICGNC 2022. Lecture Notes in Electrical Engineering, vol 845. Springer, Singapore. https://doi.org/10.1007/978-981-19-6613-2_18
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DOI: https://doi.org/10.1007/978-981-19-6613-2_18
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