DocumentCode
1873914
Title
A self-compensation algorithm for drift of platform inertial navigation system
Author
Qu, Tiejun ; Yang, Xudong ; Tian, Ziyun
Author_Institution
Dept. of Control Sci. & Eng., Harbin Inst. of Technol.
fYear
2006
fDate
19-21 Jan. 2006
Lastpage
104
Abstract
In order to improve precision of navigation of platform inertial navigation system (PINS), a self-compensation algorithm for drift of PINS is given in this paper. According to characters of this disturbance torques acting on stable shaft of platform and moving shaft of gyroscope, they are classified detailed and first described by model parameters completely reflecting their movement law in time domain, the function relation from these model parameters to output signal of gyroscope is established. An effective float encoding genetic algorithm (FGA) is designed, and then these model parameters are identified by FGA and further used to compensate the disturbance torques acting on moving shaft of gyroscope for ultimately improving the system precision. The proposed method only applies output signal of gyroscope fixed on platform as reference signal, therefore this method is a self-compensation scheme for drift of platform. A simulation example demonstrated the efficiency of the proposed approach
Keywords
error compensation; genetic algorithms; gyroscopes; inertial navigation; modelling; torque; disturbance torques; float encoding genetic algorithm; gyroscope drift; model parameters; navigation precision; platform inertial navigation system; self-compensation algorithm; Evolution (biology); Genetic algorithms; Genetic mutations; Gyroscopes; Inertial navigation; Mathematical model; Parameter estimation; Pins; Shafts; Signal processing;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems and Control in Aerospace and Astronautics, 2006. ISSCAA 2006. 1st International Symposium on
Conference_Location
Harbin
Print_ISBN
0-7803-9395-3
Type
conf
DOI
10.1109/ISSCAA.2006.1627711
Filename
1627711
Link To Document