[1]BAR-ITZHACK I Y, HARMAN R R. Optimized TRIAD algorithm for attitude determination, Journal of Guidance[J], Control, and Dynamics, 1997, 20(1):208~211 [2]FARRELL J L, STUELPNAGEL J C, WESWNER R H, WELMAN J R and BROCK J E. “A Least Squares Estimate of Spacecraft Attitude” SIAM Review[C], Vol.8, No.3, July 1966, pp. 384-386 [3]DAVENPORT P B. A Vector Approach to the Algebra of Rotations with Applications[C]. NASA X-546-65-437, November 1965. [4]BLACK H D A Passive System for Determining the Attitude of a Satellite[C]. AIAA Journal, Vol.2, No.7, July 1964, 1350-1351. [5]Wahba G. “A Least Squares Estimate of Satellite Attitude, Problem 65.1,” SIAM Review[C], July 1966, pp. 385-386. [6]Markley F L. Attitude determination Using Vector Observation and the Singular Value decomposition [J]. Journal of the Astronautical Sciences (S0021-9142). 1988, 36(3): 245-258. [7]Markley F L. Attitude determination Using Vector Observation: A Fast Optimal Matrix Algorithm [J]. Journal of the Astronautical Sciences(S0021-9142). 1993, 41(2): 261-281. [8]Keat J. Analysis of Least-Square Attitude Determination Routine, DOAOP[R], Computer Science Corp., Report CSC/TM77/6034,Feb.1977 [9]程国采. 四元数法及其应用[M],国防科技大学出版社,1991.11,长沙 [10]Lu G. Development of a GPS Multi-Antenna System for Attitude Determination[D], PhD Thesis(1995), The university of Calgary, Calgary , Canada. |