Optics and Precision Engineering, Volume. 22, Issue 3, 569(2014)
Determination of ship attitude based on dual star sensors
[1] [1] LIEBE C C.Accuracy performance of star tracker-a tutorial[C].IEEE Transactions on Aerospace and Electronic Systems, 2002, 38(2): 557-59.
[2] [2] BLARRE L.QUAKINE J.et al..High accuracy sodern star trackers: recent improvements proposed on SED36 and HYDRA star trackers[C].AIAA Guidance, Navigation, and Conference and Exhibition, AIAA, 2006: 6046.
[3] [3] MORTARI D, ROMOLI A.Starnav III: a three field of view star tracker[J].IEEE Aerospace Conference Proceeding, 2002, 1: 47-57.
[4] [4] LIU CH SH, XIAO S, MA T, et al..Attitude determination of missile based on dual FOVS sensor[J].Infrared and Laser Engineering, 2007, 36 (supp.): 540-543.(in Chinese)
[6] [6] WEI X G, ZHANG G J, FAN Q Y, et al..On-orbit calibration of star sensor based on radial alignment constraint[J].Opt. Precision Eng., 2008, 16(10): 2009-2011.(in Chinese)
[8] [8] MA W ZH. The Tutorial of Celestial Astronomy[M].Beijing: Normal Univ. Press, 1995.(in Chinese)
[9] [9] MAO Y X, ZHANG T SH, ZHU W K, et al..A real-time atmospheric refraction correction method for measurement data of ship-borne star sensors[J].Journal of Spacecraft TT&C Technology, 2012, 31(3): 50-53.(in Chinese)
[10] [10] KUDVA P, THROCKMORTON A.Attitude determination studies for the earth observation system AM1(EOS-AM1)mission[J].AIAA Journal of Guidance, Control, and Dynamics, 1996, 19(6): 1326-1331.
[11] [11] SHUSTER M D, OH S D.Three-axis attitude determination from vector observation[J].AIAA Journal of Guidance and Control, 1981, 4(1): 70-77.
[12] [12] RENE A.Stellar attitude determination accuracy with multiple star tracking advanced star tracker[J].SPIE, 1993, 1949(19): 216-227.
Get Citation
Copy Citation Text
LIU Bing, ZHU Wei-kang, ZHANG Tong-shuang, YANG Lei, GUO Jing-ming. Determination of ship attitude based on dual star sensors[J]. Optics and Precision Engineering, 2014, 22(3): 569
Category:
Received: May. 8, 2013
Accepted: --
Published Online: Apr. 24, 2014
The Author Email: Tong-shuang ZHANG (zts_123@163.com)