Kalman filtering using the quaternion extracted from vector measurements

Advances in the Astronautical Sciences

Volumn 108 I, Issue , 2001, Pages 571-586

  Kim, Injung ^a   Kim, Jinho ^a   Lim, Samsung ^a  

^a Inha University   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; EIGENVALUES AND EIGENFUNCTIONS; ERROR ANALYSIS; MATRIX ALGEBRA; SATELLITES;

QUATERNIONS; SINGLE POINT ATTITUDE DETERMINATION;

KALMAN FILTERING;

EID: 0035732245     PISSN: 10816003     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

1. A least squares estimate of spacecraft attitude
2. Attitude determination using vector observation and the singular value decomposition
3. Three-axis attitude determination
4. Three-axis attitude determination from vector observations
5. ESOQ: A closed-form solution to the wahba problem
6. A simple Kalman filter and smoother for spacecraft attitude
7. REQUEST - A recursive QUEST algorithm for sequential attitude determination
8. Kalman filtering for spacecraft attitude estimation
9. Kalman filtering of spacecraft attitude and the QUEST model
10. Software-in-the-loop for attitude determination and control system using simulink and real-time workshop