Innovative estimation method with measurement likelihood for all-accelerometer type inertial navigation system

被引:32
作者
Lee, SC [1 ]
Huang, YC [1 ]
机构
[1] Chung Cheng Inst Technol, Dept Syst Engn, Tao Yuan 33509, Taiwan
关键词
D O I
10.1109/7.993257
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This work presents an innovative estimation scheme to solve the initial and divergent problems for an all-accelerometer inertial navigation system (INS). The proposed system uses six accelerometers mounted diagonally on each surface of a cubic. The system proposed herein exploits additional information involving the gravity effect, allowing us to determine the angular velocity. It also provides an upper bound value to initiate the platform attitude. In addition, an estimation algorithm using the own-ship trajectory estimator providing a measurement likelihood is proposed. A simulation case for estimating position and velocity of the vehicle is investigated by this approach. Results confirm the effectiveness of this information infusing concept in obtaining a convergent INS state estimation.
引用
收藏
页码:339 / 346
页数:8
相关论文
共 15 条
[1]   UTILIZATION OF MODIFIED POLAR COORDINATES FOR BEARINGS-ONLY TRACKING [J].
AIDALA, VJ ;
HAMMEL, SE .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1983, 28 (03) :283-294
[2]  
ALGRAIN MC, 1991, SPIE, V1482
[3]  
[Anonymous], 1999, SPRINGER SERIES INFO
[4]  
BARITZHAXK IY, 1993, 2 MISCONCEPTS THEORY, P1067
[5]   GYROSCOPE FREE STRAPDOWN INERTIAL MEASUREMENT UNIT BY 6 LINEAR ACCELEROMETERS [J].
CHEN, JH ;
LEE, SC ;
DEBRA, DB .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1994, 17 (02) :286-290
[6]  
DINAPOLI LD, 1965, THESIS U PENNSYLVANI
[7]  
Franklin G. F., 1997, DIGITAL CONTROL DYNA
[8]  
Greenwood DT., 1988, PRINCIPLES DYNAMICS
[9]   BEARINGS-ONLY TRACKING - A HYBRID COORDINATE SYSTEM APPROACH [J].
GROSSMAN, W .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1994, 17 (03) :451-457
[10]   OBSERVABILITY REQUIREMENTS FOR 3-DIMENSIONAL TRACKING VIA ANGLE MEASUREMENTS [J].
HAMMEL, SE ;
AIDALA, VJ .
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1985, 21 (02) :200-207