New approach to attitude determination using global positioning system carrier phase measurements

Journal of Guidance, Control, and Dynamics

Volumn 25, Issue 1, 2002, Pages 130-136

  Li, Yong ^a,c   Murata, Masaaki ^a,c   Sun, Baoxiang ^b,d  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b BEIJING INSTITUTE OF CONTROL ENGINEERING   (China)

^c Jindaiji higashi machi ^*  (Japan)

^d Division of ControlSystem Design and Dynamics Simulation   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; ANTENNAS; COMPUTATIONAL METHODS; GLOBAL POSITIONING SYSTEM; ITERATIVE METHODS; MATRIX ALGEBRA; PHASE MEASUREMENT;

ATTITUDE MATRIX ELEMENT SOLUTION (AMES);

AIR NAVIGATION;

EID: 0036152178     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4857     Document Type: Article

References (14)

1. Attitude estimation algorithms for spinning satellites using global positioning system phase data
2. Attitude determination
3. Spacecraft attitude/rate estimation using vector-aided GPS observations
4. Two studies of high performance attitude determination using GPS: Generalizing Wahba's problem for high output rates and evaluation for static accuracy using a theodolite
5. Algorithms for attitude determination using the global positioning system
6. New algorithm for attitude determination using global positioning system signals
7. Integer ambiguity resolution of the GPS carrier for spacecraft attitude determination
8. A new motion-based algorithm for GPS attitude integer resolution
9. Global positioning system integer ambiguity resolution without attitude knowledge
10. A new method of instantaneous ambiguity resolution
11. Euler-q algorithm for attitude determination from vector observations
12. Optimized TRIAD algorithm for attitude determination
13. On the convergence of iterative orthogonalization processes