Title :
Design of inertial navigation system based on micromechanical gyroscope and accelerometer
Author :
Pingping, Qu ; Li, Fu ; Xin, Zhao
Author_Institution :
Shenyang Inst. of Aeronaut. Eng., Acad. of Electron. & Inf. Eng., Shenyang, China
Abstract :
A mini and low-cost strapdown inertial navigation system (SINS) is designed for civilian. Micromechanical gyroscope and accelerometer are the inertial measurement units. For the problem of high calculation of SINS, this paper adopts digital signal processor (DSP) and complex programmable logic device (CPLD) as the core of hardware system to realize signal acquisition and data communication. The navigation information is gained by calculating acquired data signal with strapdown inertial navigation algorithm, error compensation algorithm is researched for the variety system error, and finally the navigation precision of SINS is improved.
Keywords :
accelerometers; data communication; digital signal processing chips; gyroscopes; inertial navigation; micromechanical devices; programmable logic devices; signal detection; accelerometer; complex programmable logic device; data communication; digital signal processor; error compensation algorithm; hardware system; inertial measurement units; inertial navigation system; low-cost strapdown inertial navigation system; micromechanical gyroscope; signal acquisition; Accelerometers; Digital signal processing; Digital signal processors; Gyroscopes; Inertial navigation; Measurement units; Micromechanical devices; Programmable logic devices; Signal processing algorithms; Silicon compounds; Complex Programmable Logic Device (CPLD); Digital Signal Processor (DSP); Micromechanical Gyroscope; Strapdown Inertial Navigation System (SINS);
Conference_Titel :
Control and Decision Conference, 2009. CCDC '09. Chinese
Conference_Location :
Guilin
Print_ISBN :
978-1-4244-2722-2
Electronic_ISBN :
978-1-4244-2723-9
DOI :
10.1109/CCDC.2009.5194612
