Command Control and Simulation >
Design of Inertial/GNSS Integrated Navigation Simulation Verification System Based on MFC
Received date: 2019-10-31
Revised date: 2020-01-02
Online published: 2022-05-10
In order to verify the effectiveness of the inertial navigation system algorithm, a flight control simulation system is designed to generate flight trajectory data in line with the actual situation. The Strapdown Inertial Multi-subsample algorithm is written in Visual C++language. The SINS/GNSS integrated navigation system is designed based on the MFC modularization idea; based on UDP network, it can perform real-time navigation algorithm simulation verification. The simulation results show that the simulation verification system has good engineering application value for verifying the effectiveness of navigation algorithm and judging system performance.
XU Jing-shuo , PENG Wei-qi , XU Guo-feng . Design of Inertial/GNSS Integrated Navigation Simulation Verification System Based on MFC[J]. Command Control and Simulation, 2020 , 42(3) : 74 -80 . DOI: 10.3969/j.issn.1673-3819.2020.03.014
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