Title :
Research on Strap-down Inertial Navigation System Simulation
Author :
Liansheng, Liu ; Tao, Jia
Author_Institution :
Basic Exp. Center, Civil Aviation Univ. of China, Tianjin, China
Abstract :
In order to the features of inertial navigation, the simulation of strap down inertial navigation system is divided into four parts: flight track simulation module, gyroscope simulation module, accelerometer simulation module and Strap-down inertial navigation algorithm module. Using Simulink/Aerosim simulation toolkit for simulation of various modules, and ultimately get the position error, proved the correctness of simulation model. The signal of navigation parameters will be loaded into the physical model through the interface, after the format conversion of electrical characteristics of binding and the formation of ARINC429 signal.
Keywords :
accelerometers; aerospace simulation; gyroscopes; inertial navigation; Simulink-Aerosim simulation toolkit; accelerometer simulation module; binding electrical characteristics; flight track simulation module; gyroscope simulation module; navigation parameter; strap-down inertial navigation system simulation; Acceleration; Accelerometers; Gyroscopes; Load modeling; Mathematical model; Navigation; Silicon compounds; ARINC429; Flight Track; Simulink /Aerosim; Strap-down Inertial Navigation System;
Conference_Titel :
Intelligent Computation Technology and Automation (ICICTA), 2011 International Conference on
Conference_Location :
Shenzhen, Guangdong
Print_ISBN :
978-1-61284-289-9
DOI :
10.1109/ICICTA.2011.577