New method for extracting the quaternion from a rotation matrix

被引：85

作者：

Bar-Itzhack, IY ^{[1
]}

机构：

[1] Technion Israel Inst Technol, IL-32000 Haifa, Israel

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2000年 / 23卷 / 06期

关键词：

D O I：

10.2514/2.4654

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

An algorithm for extracting the quaternion from the corresponding direction cosine matrix (DCM) is presented. The algorithm is particularly useful to users of QUEST or those who solve the q method directly using an algorithm that computes matrix eigenvalues and eigenvectors.

引用

页码：1085 / 1087

页数：3

共 11 条

[1] ITERATIVE OPTIMAL ORTHOGONALIZATION OF STRAPDOWN MATRIX [J].

BARITZHACK, IY .

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1975, AE11 (01) :30-37

[2] DERIVATION OF QUATERNION SCHEME VIA EULER AXIS AND ANGLE [J].

GRUBIN, C .

JOURNAL OF SPACECRAFT AND ROCKETS, 1970, 7 (10) :1261-&

[3]

HORII M, 1999, J BRAZILIAN SOC MECH, V21, P99

[4]

Keat J., 1977, Technical report, Technical Report CSC/TM-77/6034

[5] SINGULARITY-FREE EXTRACTION OF A QUATERNION FROM A DIRECTION COSINE MATRIX [J].

KLUMPP, AR .

JOURNAL OF SPACECRAFT AND ROCKETS, 1976, 13 (12) :754-755

[6] NEW QUATERNION ATTITUDE ESTIMATION METHOD [J].

MARKLEY, FL .

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1994, 17 (02) :407-409

[7]

MARKLEY FL, 1999, 99427 AAS

[8]

Shepperd S. W., 1978, J. Guid. Control, V1, P223, DOI [10.2514/3.55767b, DOI 10.2514/3.55767B]

[9] 3-AXIS ATTITUDE DETERMINATION FROM VECTOR OBSERVATIONS [J].

SHUSTER, MD ;

OH, SD .

JOURNAL OF GUIDANCE AND CONTROL, 1981, 4 (01) :70-77

[10]

SHUSTER MD, 1993, J ASTRONAUT SCI, V41, P439

← 1 2 →