Initial matching method for use in gravimetric map matching in gravity-aided inertial navigation system
An inertial navigation system and initial matching technology, applied in the initial matching field of gravity map matching algorithm in gravity-assisted inertial navigation, to achieve the effect of overcoming failure and eliminating failure
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[0030] Such as figure 1 As shown, the traditional gravity-assisted inertial navigation system is generally divided into four modules: A, B, C and D. The main purpose of module A is to use the gravity field sensor carried on the carrier to measure the actual gravity field data on the carrier’s trajectory in real time; the main purpose of module B is to use the real-time data provided by the inertial navigation system on the carrier The purpose of module C is to use the matching algorithm to finally obtain the optimal position information of the carrier; the purpose of module D is to use the optimal matching position information and use information fusion technology to correct inertial data in real time. Systematic error within the guidance system.
[0031] The invention is mainly aimed at the initial alignment method of the matching algorithm in the C module, so as to improve the reliability and real-time performance of the gravity-assisted inertial navigation system.
[0032...
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