[1] [1] DONGWON J,TSIOTRAS P.A 3-DOF experimental test-bed for integrated attitude dynamics and control research[J/OL].AIAA Paper 03-5331,AIAA Guidance,Navigation and Control Conference,Austin,TX，2003.http://www.ae.gatech.edu/people/ptsiotra/papers/aiaa03a.pdf

[2] [2] SCHWARTZ J L,HALL C D.The distributed spacecraft attitude control system simulator:development,progress,plans[J/OL].2003 Flight Mechanics Symposium,2003.http://www.aoe.vt.edu/～cdhall/papers/FMS03.pdf

[3] [3] BANG W.Space Vehicle Dynamics and Control[M].American Institute of Aeronautics&Astronautics,1998

[4] [4] YOON H,TSIOTRAS P.Spacecraft adaptive attitude control and power tracking with single-gimballed variable speed control moment gyroscopes[J].AIAA J.Guidance,Control,and Dynamics,2002,25(6):1081-1090

[5] [5] LEFFERS E J,MARKLEY F L,SHUSTER M D.Kalman filtering for spacecraft attitude estimation[J].J.Guidance,Control and Dynamics,1982,5(5):417-428

[6] [6] SHUSTER M D.Kalman filtering of spacecraft attitude and the QUEST mode[J].J.the Astronautical Sciences,1990(3):377-393

[7] [7] CRASSIDIS J L,JUNKINS J L.Optimal Estimation of Dynamic Systems[M].New York:Chapman & Hall/CRC,2004:chapter 7