DocumentCode :
233507
Title :
Distributed attitude transfer alignment research based on INS/CNS integrated navigation system
Author :
Bing Hua ; Jing Yang ; Zhi Xiong ; Hai-ying Liu ; Guo-hua Kang ; Wei-xing Qian
Author_Institution :
Coll. of Astronaut., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
fYear :
2014
fDate :
28-30 July 2014
Firstpage :
136
Lastpage :
141
Abstract :
Distributed inertial sensor network possesses low cost, high fault tolerance and high reliability. Based on the configuration of the sensor network structure, the relationship between the main and child nodes´ inertial outputs is analyzed in the distributed inertial sensor network. The new method of transfer alignment is researched by distributed inertial network technology. On the condition that the carrier structure has serious deformation, the carrier deformation estimation can improve the alignment accuracy of the sub-navigation system. Therefore, the inertial measurement matching algorithm modified by Three-Axis Attitude Determination (TRIAD) algorithm is proposed to estimate carrier deformation angle. The simulation results show that the precision of the inertial information in the sub-navigation system is improved by estimating carrier deformation angle to transfer alignment.
Keywords :
aerospace control; attitude control; distributed control; inertial navigation; sensor fusion; INS-CNS integrated navigation system; TRIAD algorithm; carrier deformation estimation; distributed attitude transfer alignment; distributed inertial network technology; distributed inertial sensor network; inertial navigation system; three-axis attitude determination algorithm; transfer alignment method; Accelerometers; Aircraft; Aircraft navigation; Inertial navigation; Position measurement; Vectors; Attitude Transfer; Carrier deformation angle; Distributed inertial sensor network; Integrated Navigation System;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (CCC), 2014 33rd Chinese
Conference_Location :
Nanjing
Type :
conf
DOI :
10.1109/ChiCC.2014.6896610
Filename :
6896610
Link To Document :
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