[3] WEN J T, KREUTZ-DELGADO K. The attitude control problem[J]. IEEE Transactions on Automatic Control, 1991, 36(10): 1148-1162.
[5] LAM Q, PAL P, HU A, et al. Robust attitude control using a joint quaternion feedback regulator and nonlinear model-follower[C]//AIAA/AAS Astrodynamics Conference, San Diego, 1996: 817-827.
[6] LIZARRALDE F, WEN J T. Attitude control without angular velocity measurement a passivity approach[J]. IEEE Transactions on Automatic Control, 1996, 41(3): 468-472.
[7] WIE B, BARBA P M. Quaternion feedback for spacecraft large angle maneuvers[J]. Journal of Guidance, Control, and Dynamics, 1985, 8(3): 360-365.
[8] TAYEBI A. Unit quaternion-based output feedback for the attitude tracking problem[J]. IEEE Transactions on Automatic Control, 2008, 53(6): 1516-1520.
[9] WIE B, WEISS H, ARAPOSTATHIS A. Quarternion feedback regulator for spacecraft eigenaxis rotations[J]. Journal of Guidance, Control, and Dynamics, 1989, 12(3): 375-380.