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